EVENT AGENDA AIAA Guidance, Navigation, and Control Conference and Exhibit AIAA Atmospheric Flight Mechanics Conference and Exhibit AIAA Modeling and Simulation Technologies Conference and Exhibit AIAA/AAS Astrodynamics Specialist Conference and Exhibit

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At A Glance | 21-Aug-2006 | 22-Aug-2006 | 23-Aug-2006 | 24-Aug-2006 | All |

Program For Tuesday, 22-Aug-2006 0800 - 0900 Modeling and Simulation Conference Plenary Session Red Cloud Peak “Benefits of Model-Based Design for Aerospace System Development and Verification” Jim Tung, MathWorks Fellow Session 42- AFM-8 Aircraft Dynamics II: Hazardous Flight Regimes Arapahoe Chaired by: G. SHAH, NASA Langley Research Center, Hampton, VA, and K. DORSETT, Lockheed Martin Aeronautics Company, Aledo, TX 0900 AIAA-2006-6267 Analytical Criterion for Onset of Departure in Inertia- Coupled Roll Maneuvers of Airplanes A. Mahale and N. Ananthkrishnan, Indian Institute of Technology Bombay, Mumbai, India 0930 AIAA-2006-6268 Trailing Vortex Wake Encounters at Altitude - A Potential Flight Safety Issue? R. Nelson, University of Notre Dame, Notre Dame, IN 1000 AIAA-2006-6270 Survey of Jet Transport Incident/Accidents with Pitch- Rate Induced Abrupt Wing Stalling near the Ground A. Brown and M. Beyers, National Research Council, Ottawa, Canada 1030 AIAA-2006-6271 A Performance- Based Method for Improving Safety during Runway Maneuvers D. Zammit-Mangion, Cranfield University; University of Malta, Cranfield, Great Britain; B. Zammit and A. Sammut, University of Malta, Msida, Malta 1100 AIAA-2006-6272 A Traffic Movement Monitoring Computer for Pre- emptive Runway Conflict Detection A. Sammut and B. Zammit, University of Malta, Msida, Malta; and D. Zammit-Mangion, Cranfield University; University of Malta, Cranfield, Great Britain Session 43- AFM-9 Reentry and Aeroassist Vehicle Technology II Ten Mile Chaired by: M. WEAVER, The Aerospace Corporation, Los Angeles, CA 0900 AIAA-2006-6273 Aerothermodynamic Optimization of Re- Entry Heat Shield Shapes for a Crew Exploration Vehicle J. Johnson, R. Starkey, and M. Lewis, University of Maryland, College Park, MD 0930 AIAA-2006-6274 Multidimensional Aerothermodynamic Analysis For Planetary Probes using OLAP Cubes P. Subrahmanyam, San Jose State University , Santa Clara, CA 1000 AIAA-2006-6275 Reentry Envelope Determination Part II: Structural Failure Due To Atmospheric Heating C. Reynerson, The Boeing Company, Aurora, CO 1030 AIAA-2006-6276 An Evaluation of Ballute Entry Systems for Lunar Return Missions I. Clark, R. Braun, J. Theisinger, and G. Wells, Georgia Institute of Technology, Atlanta, GA Session 44- AFM-10 System Identification and Parameter Estimation II Divide Chaired by: R. JATEGAONKAR, DLR, German Aerospace Research Center, Braunschweig, Germany 0900 AIAA-2006-6279 Attitude Estimation Using an Accelerometer and Rate Gyro Based Device B. Chheda, A. Crassidis, and W. Walter, Rochester Institute of Technology, Rochester, NY 0930 AIAA-2006-6280 Optimal Experiment and Input Design for Flight Test Protocol Optimization C. Seren, F. Bommier, and L. Verdier, Airbus France, Toulouse, France; A. Bucharles, ONERA-DCSD, Toulouse, France; and D. Alazard, SUPAERO, Toulouse, France 1000 AIAA-2006-6281 A Neural Model of Coefficients of Forces and Moments of Aerodynamic Forces for a Turboprop Aircraft J. Manerowski and F. Zgrzywa, Air Force Institute of Technology, Warsaw, Poland; and K. Sibilski, Air Force Institute of Technology & Wroclaw University of Technology, Warsaw, Poland 1030 AIAA-2006-6282 Air Data System Calibration of T- 50/A- 50 H. Roh, Y. Park, N. Park, and I. Lee, Korea Aerospace Industries, LTD., Sacheon, South Korea 1100 AIAA-2006-6283 Aircraft Parameter Estimation Experiment Design Considering Measurement Colored Residuals N. Salis Brasil Neto, Flight Technologies ltd, São José dos Campos, Brazil; E. Hemerly, ITA/CTA - Electronic Engineering Dept., São José dos Campos, Brazil; and L. Góes, ITA/CTA - Aero and Mechanical Engineering Dept., São José dos Campos, Brazil 1130 AIAA-2006-6284 Parameter Estimation from Flight Data of a missile using Maximum Likelihood and Neural Network Method S. Singh and A. Ghosh, Indian Institute of Technology, Kanpur, India Session 45- ASC-8 Dynamic Analysis of Space Flight Missions Crestone Peak II Chaired by: T. ELLER, Astro USA, LLC, Woodland Park, CO 0900 AIAA-2006-6285 The Partition of Unity Finite Element Approach to the Stationary Fokker- Planck Equation M. Kumar, P. Singla, S. Chakravorty and J. Junkins, Texas A&M University, College Station, TX 0930 AIAA-2006-6286 Dynamic Analysis and Control of a Stewart Platform Using A Novel Automatic Differentiation Method X. Bai, J. Turner and J. Junkins, Texas A&M University, College Station, TX 1000 AIAA-2006-6288 Realistic Models for the Comet Dynamical Environment S. Byram, D. Scheeres, and M. Combi, University of Michigan, Ann Arbor, MI 1030 AIAA-2006-6289 Polyhedral Potential and Variational Integrator Computation of the Full Two Body Problem E. Fahnestock, T. Lee, M. Leok, N. McClamroch, and D. Scheeres, University of Michigan, Ann Arbor, MI Session 46- ASC-9 NASA Conjunction Assessment (Invited Session) Crestone Peak I Chaired by: D. LELEUX, NASA Johnson Space Center, Houston, TX, and L. NEWMAN, NASA Goddard Space Flight Center, Greenbelt, MD 0900 AIAA-2006-6291 Establishment and Implementation of a Close Approach Evaluation and Avoidance Process for Earth Observing System Missions L. Newman, NASA Goddard Space Flight Center, Greenbelt, MD; and M. Duncan, a.i. solutions, Inc., Lanham, MD 0930 AIAA-2006-6292 The Debris Environment Around the Earth Science Morning and Afternoon Constellations P. Demarest, a.i. solutions Inc, Lanham, MD 1000 AIAA-2006-6293 Realistic Covariance Prediction for the Earth Science Constellation M. Duncan and A. Long, a.i. solutions, Inc., Lanham, MD 1030 AIAA-2006-6294 Adapting Covariance Propagation to Account for the Presence of Modeled and Unmodeled Maneuvers C. Schiff, a.i. solutions, Inc., Lanham, MD 1100 AIAA-2006-6295 Development of a Nonlinear Probability of Collision Tool for the Earth Observing System D. McKinley, a.i. solutions, Inc., Lanham, MD 1130 AIAA-2006-6296 Satellite Breakup Risk Mitigation D. Leleux and J. Smith, Johnson Space Center, Houston, TX Session 47- ASC-10 Rendezvous and Proximity Missions Crestone Peak III Chaired by: D. SPENCER, Pennsylvania State University, University Park, PA 0900 AIAA-2006-6298 A Brief Study of Ground Controlled Orbital Rendezvous: When is Autonomy Required? D. Geller, Utah State University, Logan, UT 0930 AIAA-2006-6299 Guidance Strategy for Hyperbolic Rendezvous D. Landau and J. Longuski, Purdue University, West Lafayette, IN 1000 AIAA-2006-6300 Relative Angles- Only Navigation and Pose Estimation for Autonomous Orbital Rendezvous D. Woffinden and D. Geller, Utah State University, Logan, UT Session 48- ASC-11 Trajectory Optimization Crestone Peak IV Chaired by: D. BYRNES, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 0900 AIAA-2006-6306 Identifying Optimal Interplanetary Trajectories through a Genetic Approach C. Bessette and D. Spencer, The Pennsylvania State University, University Park, PA 0930 AIAA-2006-6307 VTVL Suborbital RLV Upper Stage's Range Maximization Y. Xu, University of Oklahoma, Norman, OK 1000 AIAA-2006-6304 On Discrete- Time Optimality Conditions for Pseudospectral Methods F. Fahroo and I. Ross, Naval Postgraduate School, Monterey, CA 1030 AIAA-2006-6308 Trajectory Options for Human Mars Missions P. Wooster, Massachusetts Institute of Technology, Cambridge, MA; R. Braun, Georgia Institute of Technology, Atlanta, GA; J. Ahn, Massachusetts Institute of Technology, Cambridge, MA; Z. Putnam, Georgia Institute of Technology, Atlanta, GA 1100 AIAA-2006-6309 Enhanced Procedures for Direct Trajectory Optimization Using Nonlinear Programming and Implicit Integration S. Paris, Boeing Phantom Works, Seattle, WA; J. Riehl, NASA Glenn Research Center, Cleveland, OH; and W. Sjauw, NASA Kennedy Space Center, Kennedy Space Center, FL 1130 AIAA-2006-6836 Explorations of low cost connections between Lissajous orbits from the Sun- Earth and Earth- Moon systems. E. Canalias and J. Masdemont, Universitat Politecnica de Catalunya, Barcelona, Spain Session 49- GNC-21 Aircraft Control Applications Quandary Peak I Chaired by: J. MITCHELL, Ohio University, Athens, OH, and L. GIULICCHI, ESA, Noordwijk, The Netherlands 0900 AIAA-2006-6310 Closed- Loop Evaluation of An Integrated Failure Identification and Fault Tolerant Control System for A Transport Aircraft J. Shin, National Institute of Aerospace, Hampton, VA; C. Belcastro and T. Khong, NASA Langley Research Center, Hampton, VA 0930 AIAA-2006-6311 Three- Stage Gradient- Based Optimization Scheme in Design of Feedback Gains Within Eurofighter Primary Control Laws N. Moritz and R. Osterhuber, European Aeronautic Defence and Space Company, Munich, Germany 1000 AIAA-2006-6312 Near- Optimal Missile Avoidance Trajectories via Receding Horizon Control J. Karelahti, K. Virtanen, and T. Raivio, Helsinki University of Technology, Espoo, Finland 1030 AIAA-2006-6313 Feasibility Study on the Control of a Generic Air Vehicle Using CMG K. Lim and D. Moerder, NASA Langley Research Center, Hampton, VA 1100 AIAA-2006-6314 Design and Evaluation of a Haptic Flight Director S. De Stigter, M. Mulder, and R. Van Paassen, Delft University of Technology, Delft, The Netherlands Session 50- GNC-22 Aircraft Modeling and Flight Control II Quandary Peak II Chaired by: R. LIND, University of Florida, Gainesville, FL, and D. DOMAN, U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH 0900 AIAA-2006-6315 Global Robust Control of Aeroelastic System Using Output Feedback K. Lee and S. Singh, University of Nevada, Las Vegas, Las Vegas, NV 0930 AIAA-2006-6316 Trajectory Control of Very Flexible Aircraft C. Shearer and C. Cesnik, University of Michigan, Ann Arbor, MI 1000 AIAA-2006-6317 Comparison of First- and Second- Order EMA Models for an Aeroservoelastic Wing with Multiple Control Surfaces Y. Teng, The Boeing Company, Long Beach, CA 1030 AIAA-2006-6318 Robust Model Predictive Control of a Feedback Linearized F- 16/MATV Aircraft Model E. van Oort, Q. Chu, and J. Mulder, Delft University of Technology, Delft, The Netherlands Session 51- GNC-23 Airport Arrival Capacity Utilization Torreys Peak II Chaired by: R. WINDHORST, NASA Ames Research Center, Moffett Field, CA, and T. MIQUEL, Direction de la Technique et de l'Innovation, Toulouse, France 0900 AIAA-2006-6320 Scheduling Aircraft Landings Under Constrained Position Shifting H. Balakrishnan, UC Santa Cruz NASA Ames Research Center, Moffett Field, CA; B. Chandran, University of California Berkeley, Berkeley, CA 0930 AIAA-2006-6321 The effects of wind on Distance- Based Self- Spacing in Arrival Streams R. Kartodikromo, M. Mulder and M. van Paassen, Delft University of Technology, Delft, The Netherlands 1000 AIAA-2006-6322 Wake Vortex Avoidance Versus Landing Capacity K. Hahn and C. Schwarz, DLR, German Aerospace Research Center, Braunschweig, Germany 1030 AIAA-2006-6323 Predicting Aircraft Approach Speeds for Enhancing Airport Capacity J. Helleberg, D. Domino, A. Mundra and R. Mayer, MITRE Corporation, McLean, VA 1100 AIAA-2006-6324 Target Tracking and Estimated Time of Arrival (ETA) Prediction for Arrival Aircraft K. Roy, Stanford University, Stanford, CA; B. Levy, Sensis Corporation, Dewitt, NY; C. Tomlin, Stanford University, Stanford, CA Session 52- GNC-24 Control and Vibration Suspension of Aeroservoelastic Systems Quandary Peak III Chaired by: P. GURFIL, Technion - Israel Institute of Technology, Haifa, Israel, and A. TSOURDOS, Cranfield University, Wiltshire, Great Britain 0900 AIAA-2006-6326 Output Feedback Adaptive Variable Structure Control of a Smart Projectile Fin S. Mani, S. Singh, and W. Yim, University of Nevada, Las Vegas, Las Vegas, NV; and A. Araujo, Federal University of Rio Grande do Norte, Natal, Brazil 0930 AIAA-2006-6329 Neural Adaptive Vibration Suppression System for Smart Structures in Aircraft S. Suresh and P. Saratchandran, Nanyang Technological University, Singapore, Singapore; K. Natesan, University of Leicester, Leicester, Great Britain; A. Rao, Indian Institute of Science, Bangalore, India; N. Sundararajan, Nanyang Technological University, Singapore, Singapore 1000 AIAA-2006-6331 Assessment Criteria as Specifications for Reconfiguring Control T. Lombaerts, D. Joosten, Q. Chu and J. Mulder, Delft University of Technology, Delft, The Netherlands; J. Breeman, National Aerospace Laboratory/NLR, Amsterdam, The Netherlands; T. Boom, Delft University of Technology, Delft, The Netherlands Session 53- GNC-25 Dynamics and Control of Evolving Structures Torreys Peak III Chaired by: M. WHORTON, NASA Marshall Space Flight Center, Huntsville, AL, and M. BALAS, University of Wyoming, Laramie, WY 0900 AIAA-2006-6332 Evolving Systems: A Theoretical Foundation M. Balas and S. Frost, University of Wyoming, Laramie, WY; F. Hadaegh, Jet Propulsion Laboratory, Pasadena, CA 0930 AIAA-2006-6333 Evolving Systems: A Theoretical Foundation M. Balas and S. Frost, University of Wyoming, Laramie, WY; and F. Hadaegh, NASA Jet Propulsion Laboratory, Pasadena, CA 1000 AIAA-2006-6334 Mated Flight Control Issues for Space Exploration Systems K. Lim, NASA Langley Research Center, Hampton, VA; L. Markley, NASA Goddard Space Flight Center, Greenbelt, MD; and M. Whorton, NASA Marshall Space Flight Center, Huntsville, AL 1030 AIAA-2006-6336 Deployment Modeling of an Inflatable Solar Sail Spacecraft N. Graybeal and J. Craig, Georgia Institute of Technology, Atlanta, GA; and M. Whorton, NASA Marshall Space Flight Center, Huntsville, AL 1100 AIAA-2006-6337 Adaptive Control of Evolving Gossamer Structures B. Yang, A. Calise and J. Craig, Georgia Institute of Technology, Atlanta, GA; M. Whorton, NASA Marshall Space Flight Center, Huntsville, AL Session 54- GNC-26 General Aviation and Small Aircraft Guidance, Navigation, and Control Gray's Peak II Chaired by: R. COLGREN, University of Kansas, Lawrence, KS, and B. NEWMAN, Old Dominion University, Norfolk, VA 0900 AIAA-2006-6338 Descent Management Strategies for Future Small Aircraft Transportation Systems B. Newman and C. Britcher, Old Dominion University, Norfolk, VA; Y. Kassaye, The Boeing Company, Seattle, WA; J. Roy, Dynetics, Huntsville, AL; M. Krizansky, GE Aircraft Engines, Evendale, OH; and M. Acheson, NASA Langley Research Center, Hampton, VA 0930 AIAA-2006-6339 Application of Relay Tuning Methods to UAV Autopilots S. Patankar and D. Schinstock, Kansas State University, Manhattan, KS; R. Caplinger, Athena Technologies Inc, Warrenton, VA 1000 AIAA-2006-6340 Problems of Monitoring in the Fly- by- Wire System for Small Aircraft G. Kopecki and P. Rzucidlo, Rzeszow University of Technology, Rzeszow, Poland 1030 AIAA-2006-6341 Neural Network Based Adaptive Flight Control Using Feedback Error Learning R. Haga, A. Matsuura and S. Suzuki, University of Tokyo, Tokyo, Japan; M. Kono and A. Sakaguchi, Fuji Heavy Industries, Utsunomiya, Tochigi, Japan Session 55- GNC-27 Intelligent Control in Aerospace Applications I Gray's Peak I Chaired by: C. CAO and J. WANG, Virginia Polytechnic Institute and State University, Blacksburg, VA 0900 AIAA-2006-6342 Stable Adaptation in the Presence of Multiple Actuator Constraints E. Lavretsky, The Boeing Company, Huntington Beach, CA; N. Hovakimyan, Virginia Polytechnic Institute and State University, Blacksburg, VA 0930 AIAA-2006-6343 An Adaptive Approach to Nonaffine Control Design for Aircraft Applications A. Young, C. Cao, and N. Hovakimyan, Virginia Polytechnic Institute and State University, Blacksburg, VA; and E. Lavretsky, The Boeing Company, Huntington Beach, CA 1000 AIAA-2006-6344 Unfalsified Control for Slowly Varying Plants Using Fading Memory and Windowing S. Cheong and M. Safonov, University of Southern California, Los Angeles, CA 1030 AIAA-2006-6345 Adaptive Control of F/A- 18 Vertical Tail Buffeting P. Roberts, B. Yang, A. Calise, J. Craig and S. Hanagud, Georgia Institute of Technology, Loganville, GA 1100 AIAA-2006-6346 An Error Minimization Method in Adaptive Control K. Volyanskyy, A. Calise and B. Yang, Georgia Institute of Technology, Atlanta, GA; E. Lavretsky, The Boeing Company - Phantom Works, Huntington Beach, CA 1130 AIAA-2006-6347 Are Phase and Time- Delay Margins Always Adversely Affected by High- Gain? C. Cao, V. Patel, K. Reddy, and N. Hovakimyan, Virginia Polytechnic Institute and State University, Blacksburg, VA; E. Lavretsky, The Boeing Company, Huntington Beach, CA; and K. Wise, Virginia Polytechnic Institute and State University, Blacksburg, VA Session 56- GNC-28 Navigation and Estimation Gray's Peak III Chaired by: T. KIM, Sandia National Laboratories, Albuquerque, NM, and J. HUI, Charles Stark Draper Laboratory, Inc., Cambridge, MA 0900 AIAA-2006-6348 Generalizations of the Complex- Step Derivative Approximation K. Lai and J. Crassidis, University at Buffalo, Amherst, NY 0930 AIAA-2006-6349 Derivation and Simulation Testing of a Sigma- Points Smoother M. Psiaki, Cornell University, Ithaca, NY; and M. Wada, University of Tokyo, Tokyo, Japan 1000 AIAA-2006-6350 Neural Network Augmented Kalman Filtering in the Presence of Unknown System Inputs R. Sattigeri and A. Calise, Georgia Institute of Technology, Atlanta, GA 1030 AIAA-2006-6351 Development of UAV Navigation System Based on Unscented Kalman Filter S. Oh and E. Johnson, Georgia Institute of Technology, Atlanta, GA 1100 AIAA-2006-6352 Unscented Kalman Filtering: NPSAT1 Ground Test Results P. Sekhavat, Q. Gong and I. Ross, Naval Postgraduate School, Monterey, CA 1130 AIAA-2006-6353 UKF Based In- Flight Alignment Using Low Cost IMU C. Park, K. Kim and W. Kang, Seoul National University, Seoul, South Korea Session 57- GNC-29 Robust and Optimal Aircraft Control II Torreys Peak I Chaired by: A. CALISE, Georgia Institute of Technology, Atlanta, GA, and Y. BEN-ASHER, Technion - Israel Institute of Technology, Haifa, Israel 0900 AIAA-2006-6354 Pseudospectral Feedback Control: Foundations, Examples and Experimental Results I. Ross, P. Sekhavat, A. Fleming, Q. Gong and W. Kang, Naval Postgraduate School, Monterey, CA 0930 AIAA-2006-6355 A New Approach for Control of Periodically Time Varying Systems with Application to Spacecraft Momentum Unloading S. Kalender and H. Flashner, University of Southern California, Los Angeles, CA 1000 AIAA-2006-6356 Multiple- Model Design of Robustified Repetitive Controllers with Optimized Convergence Rate S. Lee, Daegu University, Daegu, South Korea; M. Phan, Dartmouth College, Hanover, NH; R. Longman, Columbia University, New York, NY 1030 AIAA-2006-6357 Simultaneous Stabilization of Linear Plants Using a Multidisciplinary Design Optimization Analogy R. Perez and H. Liu, University of Toronto, Toronto, Canada; and K. Behdinan, Ryerson University, Toronto, Canada 1100 AIAA-2006-6358 Direct Trajectory Optimization and Costate Estimation via an Orthogonal Collocation Method D. Benson, G. Huntington, T. Thorvaldsen, and A. Rao, Charles Stark Draper Laboratory, Inc., Cambridge, MA 1130 AIAA-2006-6359 On Synergetic Extremal Control for Aerospace Applications A. Nusawardhana and W. Crossley, Purdue University, West Lafayette, IN Session 58- MST-8 Motion Systems: Architectures and Design Tools Castle Peak I Chaired by: S. ADVANI, Aircraft Development and Systems Engineering, Breda, The Netherlands 0900 AIAA-2006-6360 Study of a Novel Motion Platform for Flight Simulators Using an Anthropomorphic Robot L. Pollini and M. Innocenti, University of Pisa, Pisa, Italy; and A. Petrone, QDesign SRL, Pisa, Italy 0930 AIAA-2006-6361 Improved Position Accuracies of Multi- Axis Motion Test Simulators R. Mitchell and J. Marchetti, Ideal Aerosmith Incorporated, Pittsburgh, PA 1000 AIAA-2006-6362 Detailed Dynamic Modeling of the NASA LaRC CMF Motion Base D. Carrelli, Swales Aerospace Inc., Hampton, VA 1030 AIAA-2006-6363 Software Tools for Developing and Simulating the NASA LaRC CMF Motion Base R. Bryant, NASA Langley Research Center, Hampton, VA; and D. Carrelli, Swales Aerospace Inc., Hampton, VA 1100 AIAA-2006-6364 Evaluating the Performance of the NASA LaRC CMF Motion Base Safety Devices L. Gupton and R. Bryant, NASA Langley Research Center, Hampton, VA; and D. Carrelli, Swales Aerospace Inc., Hampton, VA Session 59- MST-9 Threat, Weapons, and Engagement Modeling and Simulation Castle Peak II Chaired by: F. WELLER, Northrop Grumman Corporation, Alexandria, VA 0900 AIAA-2006-6365 The Air Combat Lab a Modular Air- to- Air Combat Simulation C. Mentz, F. Holzapfel, W. Längler, and M. Strohal, Industrieanlagen Betriebsgesellschaft mbH, Ottobrunn, Germany 0930 AIAA-2006-6366 Integration and Optimization of Projectile Design Models A. Farina, US Army Armament Research, Development and Engineering Center, Picatinny Arsenal, NJ; C. Chassapis, Stevens Institute of Technology, Hoboken, NJ; and Y. Chen, US Army Armament Research, Development and Engineering Center, Picatinny Arsenal, NJ 1000 AIAA-2006-6367 Neural Model of Antiaircraft Missile Flight Control D. Karczmarz, J. Manerowski and C. Szczepanski, Air Force Institute of Technology, Warsaw, Poland Session 77- MST-12 Flight Simulator Subsystems and Architectures Castle Peak III Chaired by: R. SLYWCZAK, NASA Glenn Research Center, Cleveland, OH 0900 AIAA-2006-6477 GRACE – a Versatile Simulator Architecture Making Simulation of Multiple Complex Aircraft Simple B. Heesbeen, R. Ruigrok, and J. Hoekstra, National Aerospace Laboratory NLR, Amsterdam, The Netherlands 0930 AIAA-2006-6478 General Aviation Data Framework E. Blount, Unisys Corporation, NASA Langley Research Center, Hampton, VA; and V. Chung, NASA Langley Research Center, Hampton, VA 1000 AIAA-2006-6479 Deterministic Data Access and Manipulation in Simulators with a VxWorks Target W. Davidson and G. Tupa, United Space Alliance, LLC, Houston, TX 1200 - 1400 Awards Luncheon Red Cloud Peak "Stardust - Bringing a Comet Home" Joseph M. Vellinga, Lockheed Martin Corporation Session 61- AFM-11 Atmospheric Flight Mechanics Education Workshop Torreys Peak IV Chaired by: E. FIELD, The Boeing Company, Huntington Beach, CA, and J. VALASEK, Texas A&M University, College Station, TX 1400 AIAA-2006-6824 Atmospheric Flight Mechanics Education - Are the Customers Getting What They Need? E. Field, The Boeing Company, Phantom Works, Huntington Beach, CA Session 62- AFM-12 Linear and Nonlinear Equations of Motion Torreys Peak III Chaired by: R. CLARKE, NASA Dryden Flight Research Center, Edwards, CA 1400 AIAA-2006-6370 The Bifurcation Tailoring for Nonlinear Entomopter Control K. Sibilski, Air Force Institute of Technology and Wroclaw Technical University of Wroclaw, Faculty of Mechanics and Power Engineering, Warsaw, Poland 1430 AIAA-2006-6371 Alternative Derivation of the Euler Axis Kinematic Differential Equation Using Eigensystem Derivatives B. Burchett, Rose-Hulman Institute of Technology, Terre Haute, IN 1500 AIAA-2006-6372 A Dynamic Performance Evaluation Technique for Unmanned Aerial Vehicles M. Sadraey and R. Colgren, University of Kansas, Lawrence, KS 1530 AIAA-2006-6374 Periodic Solutions for Flexible Cable- Body Systems Towed in Circular and Elliptical Paths P. Williams and P. Trivailo, RMIT University, Melbourne, Australia 1600 AIAA-2006-6375 Dynamics and Equilibrium of a Twin- Aircraft- Cable System for Payload Retrieval P. Williams and P. Trivailo, RMIT University, Bundoora, Australia Session 63- AFM-13 Public Safety in Spacecraft Launch and Reentry Operations I Castle Peak IV Chaired by: L. BONAPARTE and D. MURRAY, Federal Aviation Administration, Washington, DC 1400 AIAA-2006-6378 A Tool for Integrating Commercial Space Operations into the National Airspace System D. Murray, Federal Aviation Administration, Washington, DC; and R. VanSuetendael, Federal Aviation Administration, Kennedy Space Center, FL 1430 AIAA-2006-6379 A Strategy for Reducing Hazards from Reentry Debris W. Ailor, The Aerospace Corporation, El Segundo, CA; L. Bonaparte, FAA Office of Commercial Space Transportation, Washington, DC; and A. Shelton, USAF Space and Missile Systems Center, El Segundo, CA 1500 AIAA-2006-6500 Hazard Analysis for Uncontrolled Space Vehicle Reentry R. Patera, The Aerospace Corporation, Los Angeles, CA 1530 AIAA-2006-6381 Guided Weapon Danger Area Generation – Implementing A Probabilistic Approach D. Fletcher, Defence Science and Technology Organisation, Adelaide, Australia; S. Wilson, Aerospace Concepts Pty Ltd., Canberra, Australia; M. Jokic, Defence Science and Technology Organisation, Adelaide, Australia; and I. Vuletich, Aerospace Concepts Pty Ltd., Canberra, Australia 1600 AIAA-2006-6826 Response of Graphite/Epoxy Structures to the Reentry Environment W. Ailor, R. Baker, W. Hallman, D. Moody, G. Steckel, and M. Weaver, The Aerospace Corporation, El Segundo, CA; and L. Bonaparte, Federal Aviation Administration, DC Session 64- ASC-12 Attitude Sensors and Calibration Crestone Peak IV Chaired by: M. PITTELKAU, Aerospace Control Systems, LLC, Ellicott City, MD 1400 AIAA-2006-6382 Attitude Estimation for Sounding Rockets using MEMS gyros J. Bekkeng, University of Oslo, Oslo, Norway; M. Psiaki, Cornell University, Ithaca, NY 1430 AIAA-2006-6383 Autonomous Star Tracker Performance for the New Horizons Mission G. Rogers, M. Schwinger, J. Kaidy, and T. Strikwerda, The Johns Hopkins University Applied Physics Laboratory, Laurel, MD; R. Casini, A. Landi, R. Bettarini, and S. Lorenzini, Galileo Avionica, Florence, Italy 1500 AIAA-2006-6384 Attitude Error From Phase Center Uncertainty in an Interferometric GPS Antenna Array A. Treder, Barrios Technology, Kent, WA 1530 AIAA-2006-6386 Iterative Magnetometer Calibration J. Sedlak, a.i. solutions Inc., Lanham, MD 1600 AIAA-2006-6387 Design of an Image Motion Compensation (IMC) Algorithm for the Communication, Ocean, and Meteorological Satellite (COMS) T. Jung, U. Lee, and S. Park, Yonsei University, Seoul, South Korea; Y. Choi and H. Bang, Korea Advanced Institute of Science and Technology, Daejeon, South Korea; G. Ju and K. Yang, Korea Aerospace Research Institute, Daejeon, South Korea Session 65- ASC-13 New Perspectives on the Satellite Drag Environments of Earth, Mars, and Venus II Crestone Peak II Chaired by: F. LEMOINE, NASA Goddard Space Flight Center, Greenbelt, MD, and J. FORBES, University of Colorado, Boulder, CO 1400 AIAA-2006-6390 Calculation of Zonal Winds Using Accelerometer and Rate Data from Mars Global Surveyor D. Baird, California Institute of Technology, Pasadena, CA; R. Tolson, North Carolina State University, Hampton, VA; and S. Bougher, University of Michigan, Ann Arbor, MI 1430 AIAA-2006-6391 Atmospheric density during the aerobraking of Mars Odyssey from radio tracking data E. Mazarico and M. Zuber, Massachusetts Institute of Technology, Cambridge, MA; F. Lemoine and D. Smith, Solar System Exploration Division NASA Goddard Space Flight Center, Greenbelt, MD 1500 AIAA-2006-6392 Mars Thermospheric Winds from MGS and Odyssey Accelerometers G. Crowley, Atmospheric and Space Technology Research Associates, San Antonio, TX; and R. Tolson, North Carolina State University, Raleigh, NC 1530 AIAA-2006-6393 Variability of the Satellite Drag Environments of Earth, Mars and Venus due to Rotation of the Sun J. Forbes, University of Colorado, Boulder, CO; S. Bruinsma, Centre Nationale D’Etudes Spatiales, Toulouse, France; F. Lemoine, NASA Goddard Space Flight Center, Greenbelt, MD; B. Bowman, U.S. Air Force Space Command, Colorado Springs, CO; and A. Konopliv, California Institute of Technology, Pasadena, CA 1600 AIAA-2006-6394 Global Reference Atmospheric Models, Including Thermospheres, for Mars, Venus and Earth H. Justh, NASA, Marshall Space Flight Center, AL; C. Justus, Morgan Research Corporation, Huntsville, AL; and V. Keller, NASA, Marshall Space Flight Center, AL 1630 AIAA-2006-6395 Thermospheric Studies with Mars Global Surveyor F. Lemoine, NASA Goddard Space Flight Center, Greenbelt, MD; S. Bruinsma, Centre Nationale D’Etudes Spatiales, Toulouse, France; D. Chinn, SGT Inc., Greenbelt, MD; and J. Forbes, University of Colorado, Boulder, CO 1700 AIAA-2006-6396 Method for Deriving Densities and In- Track Winds During Storms K. Moe and M. Moe, Space Environment Technologies, Irvine, CA 1730 AIAA-2006-6397 Application of MGS and ODY Aerobraking Accelerometer Data to Atmospheric Modeling R. Tolson, North Carolina State University, Hampton, VA; G. Keating, The George Washington University, Newport News, VA; R. Zurek, California Institute of Technology, Pasadena, CA; S. Bougher, University of Michigan, Ann Arbor, MI; C. Justus, Morgan Research Corp., Huntsville, AL; and D. Fritts, NorthWest Research Associates, Inc., Boulder, CO Session 66- ASC-14 Orbit Determination and Tracking I Crestone Peak I Chaired by: J. SEAGO, Analytical Graphics, Inc., Exton, PA 1400 AIAA-2006-6398 Covariance Analysis of Cassini Titan Flyby using SAR and Altimetry Data R. Park, The University of Michigan, Ann Arbor, MI; L. Cangahuala, P. Chodas, and I. Roundhill, Jet Propulsion Laboratory, Pasadena, CA 1430 AIAA-2006-6399 Nonlinear Semi- Analytic Method for Spacecraft Navigation R. Park and D. Scheeres, University of Michigan, Ann Arbor, MI 1500 AIAA-2006-6401 MR SAT Orbit Determination Using the 0- D Filter M. Dancer, J. Searcy and H. Pernicka, University of Missouri - Rolla, Rolla, MO 1530 AIAA-2006-6402 Towards the GEOSAT Follow- On Precise Orbit Determination Goals of High Accuracy and Near- Real- Time Processing F. Lemoine, NASA Goddard Space Flight Center, Greenbelt, MD; N. Zelensky, D. Chinn and B. Beckley, SGT Inc., Greenbelt, MD; J. Lillibridge, National Oceanic and Atmospheric Administration, Silver Spring, MD 1600 AIAA-2006-6403 Orbit Determination for Microscope satellite scientific purpose S. Delavault and F. Mercier, Centre Nationale D’Etudes Spatiales, Toulouse, France Session 67- ASC-15 Stardust Navigation (Invited Session) Crestone Peak III Chaired by: K. WILLIAMS and A. CANGAHUALA, Jet Propulsion Laboratory, Pasadena, CA 1400 AIAA-2006-6406 Maneuver Analysis and Targeting Strategy for the Stardust Re- Entry Capsule C. Helfrich, R. Bhat, J. Kangas, R. Wilson, M. Wong, C. Potts, and K. Williams, Jet Propulsion Laboratory, Pasadena, CA 1430 AIAA-2006-6408 Modeling of Deadbanding Delta- V for the Stardust Earth Return: Calibration, Analysis, Prediciton and Performance B. Kennedy, T. McElrath, and S. Nandi, California Institute of Technology, Pasadena, CA 1500 AIAA-2006-6409 On- Orbit Maneuver Calibrations for the Stardust Spacecraft S. Nandi, B. Kennedy, K. Williams, and D. Byrnes, California Institute of Technology, Pasadena, CA 1530 AIAA-2006-6410 Entry, Descent, and Landing Operations Analysis for the Stardust Re- Entry Capsule P. Desai, NASA Langley Research Center, Hampton, VA; D. Lyons, J. Tooley, and J. Kangas, Jet Propulsion Laboratory, Pasadena, CA 1600 AIAA-2006-6411 Interfacing with USSTRATCOM and UTTR During Stardust Earth Return D. Jefferson, D. Baird, L. Cangahuala, and G. Lewis, California Institute of Technology, Pasadena, CA 1630 AIAA-2006-6412 Stardust Entry: Landing and Population Hazards in Mission Planning and Operations J. Tooley and D. Lyons, California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA; P. Desai, NASA Langley Research Center, Hampton, VA; and G. Wawrzyniak, Purdue University, West Layfayette, IN Session 68- GNC-30 Adaptive Aircraft Control Gray's Peak II Chaired by: M. BALAS, University of Wyoming, Laramie, WY, and D. DIGGLE, Ohio University, Athens, OH 1400 AIAA-2006-6413 Constrained Adaptive Backstepping Flight Control: Application to a Nonlinear F- 16/MATV Model L. Sonneveldt, Q. Chu, and J. Mulder, Delft University of Technology, Delft, The Netherlands 1430 AIAA-2006-6414 Adaptive Disturbance Rejection Control Using System Input- Output Data N. Kulkarni, QSS Group Inc., NASA Ames Research Center, Moffett Field, CA 1500 AIAA-2006-6415 An Adaptive Flight Controller Using Growing and Pruning Radial Basis Function Network P. Shankar and R. Yedavalli, Ohio State University, Columbus, OH; and J. Burken, NASA Dryden Flight Research Center, Edwards, CA 1530 AIAA-2006-6416 Theoretically Verifiable Stability Margins for an Adaptive Controller Z. Dydek, H. Jain, J. Jang, and A. Annaswamy, Massachusetts Institute of Technology, Cambridge, MA; and E. Lavretsky, The Boeing Company, Huntington Beach, CA 1600 AIAA-2006-6417 Theoretical Stability Analysis of Simple Adaptive Control for a Winged Re- Entry Vehicle E. Mooij, Dutch Space BV, Leiden, The Netherlands; and I. Barkana, Kulicke and Soffa Industries, Inc., Willow Grove, PA Session 69- GNC-31 Control Theory and Applications Quandary Peak I Chaired by: D. IRWIN, Ohio University, Athens, OH, and M. ROSS, Naval Postgraduate School, Monterey, CA 1400 AIAA-2006-6418 Stability Analysis of Switched Dynamical Systems with State- Space Dilation and Contraction P. Wang, University of California, Los Angeles, Los Angeles, CA; and F. Hadaegh, Jet Propulsion Laboratory, Pasadena, CA 1430 AIAA-2006-6419 Decentralized Predictive Control for Tracking and Disturbance Rejection R. Darling and M. Phan, Dartmouth College, Hanover, NH 1500 AIAA-2006-6420 Predictive Control of Unmeasured Outputs R. Darling, Dartmouth College, Bradford, VT; and M. Phan, Dartmouth College, Hanover, NH 1530 AIAA-2006-6421 Direct Data- Based Model Predictive Controller Design J. Barlow and M. Phan, Dartmouth College, Hanover, NH 1600 AIAA-2006-6422 Output Regulation with Bounded Control for the Benchmark Active Control Technology Model E. Applebaum and J. Ben-Asher, Technion—Israel Institute of Technology, Haifa, Israel 1630 AIAA-2006-6423 Linear Feedback Control Using Quasi Velocities A. Sinclair, Auburn University, Auburn, AL; J. Hurtado and J. Junkins, Texas A&M University, College Station, TX 1700 AIAA-2006-6425 Game- Theoretic Modeling and Control of Military Air Operations with Civilian Players M. Wei, Ohio State University, Columbus, OH; G. Chen, Intelligent Automation, Inc., Rockville, MD; J. Cruz, Ohio State University, Columbus, OH; C. Kwan, Intelligent Automation, Inc., Rockville, MD; and M. Kruger, Office of Naval Research, Arlington, VA Session 70- GNC-32 Intelligent Control in Aerospace Applications II Torreys Peak I Chaired by: C. CAO and J. WANG, Virginia Polytechnic Institute and State University, Blacksburg, VA 1400 AIAA-2006-6426 Application of L1 Adaptive Controller to Wing Rock C. Cao and N. Hovakimyan, Virginia Polytechnic Institute and State University, Blacksburg, VA; and E. Lavretsky, The Boeing Company, Huntington Beach, CA 1430 AIAA-2006-6427 Autonomous Rover Control with Behavioral Algorithms and Neural Networks G. Giardini, M. Massari, and F. Bernelli, Politecnico di Milano, Milan, Italy; and M. Vasile, University of Glasgow, Glasgow, Great Britain 1500 AIAA-2006-6428 Neural Network Estimator for Closed- Loop Control of a Cylinder Wake Y. Shin, K. Cohen, S. Siegel, J. Seidel, and T. McLaughlin, U.S. Air Force Academy, Colorado Springs, CO 1530 AIAA-2006-6429 Continuous Adaptive Critic Flight Control Aided with Approximated Plant Dynamics E. van Kampen, Q. Chu and J. Mulder, Delft University of Technology, Delft, The Netherlands 1600 AIAA-2006-6430 A 1- DOF Wind Tunnel Experiment in Adaptive Flow Control A. Kutay, A. Calise and J. Muse, Georgia Institute of Technology, Atlanta, GA 1630 AIAA-2006-6431 Neuro- Adaptive Approach for Fading Actuation Accommodation in Space Flight Vehicles S. Kanury and Y. Song, North Carolina A&T State University, Greensboro, NC Session 71- GNC-33 Missile Guidance II Gray's Peak I Chaired by: J. EVERS, U.S. Air Force Research Laboratory, Eglin AFB, FL 1400 AIAA-2006-6432 Guidance Laws for Anti- Ship Missiles Using Impact Angle and Impact Time B. Jung and Y. Kim, Seoul National University, Seoul, South Korea 1430 AIAA-2006-6433 Agility vs. Stability in Homing Missiles S. Gutman and O. Ben-Aharon, Technion—Israel Institute of Technology, Haifa, Israel 1500 AIAA-2006-6439 Higher Order Statistics and the Adjoint Method for guidance loop analysis M. Weiss and D. Beld, TNO, Defence, Security and Safety, The Hague, The Netherlands Session 72- GNC-34 Modeling and Control of High-Speed Underwater Vehicles Torreys Peak II Chaired by: G. BALAS, University of Minnesota, Minneapolis, MN, and J. DZIELSKI, Pennsylvania State University, State College, PA 1400 AIAA-2006-6440 Overview of the ONR Supercavitating High- Speed Bodies Program K. Ng, Office of Naval Research, Arlington, VA 1415 AIAA-2006-6441 High- Speed Control Supercavitating Vehicles J. Dzielski, Pennsylvania State University, State College, PA; R. Kunz and R. Cook, , ; and D. David, Stinebring, 1500 AIAA-2006-6442 Overview of High- Speed Supercavitating Vehicle Control I. Kirschner, J. Uhlman and J. Perkins, Engineering Technology Center, Middletown, RI 1530 AIAA-2006-6443 Experimental Studies in the Control of Cavitating Bodies R. Kuklinski, Naval Undersea Warfare Center, Newport, RI 1600 AIAA-2006-6444 Application of Robust State and Parameter Estimation to a Supercavitating Torpedo Model N. Richards and J. Monaco, Barron Associates, Charlottesville, VA; C. Knospe, University of Virginia, Charlottesville, VA 1630 AIAA-2006-6445 Nonlinear Dynamics and Control of Supercavitating Bodies G. Lin, B. Balachandran and E. Abed, University of Maryland, College Park, MD 1700 AIAA-2006-6446 High- Speed Supercavitation Vehicle Control B. Vanek, J. Bokor and G. Balas, University of Minnesota, Minneapolis, MN Session 73- GNC-35 Spacecraft Sensing and Attitude Control I Quandary Peak II Chaired by: C. MCCORMICK, Broad Reach Engineering, Golden, CO, and S. DUSSY, ESA, Noordwijk, The Netherlands 1400 AIAA-2006-6447 Complementary Roll/Yaw Attitude Controller for Three Axis Authority Momentum Spacecraft S. Lim, Charles Stark Draper Laboratory, Inc., Cambridge, MA 1430 AIAA-2006-6448 Attitude Determination and Control Subsystem Hardware in the Loop Test on Air Bearing Trolley W. Soh and N. Hamzah, Astronautic Technology Sdn Bhd, Shah Alam, Selangor, Malaysia; W. Steyn, University of Stellenbosch, Stellenbosch, South Africa 1500 AIAA-2006-6450 Studies on Magnetic Attitude Control System for the REIMEI Microsatellite S. Sakai, Y. Fukushima, and H. Saito, Japan Aerospace Exploration Agency, Sagamihara-shi, Japan; and R. Kaneda, University of Tokyo, Bunkyo, Japan Session 74- GNC-36 UAV Cooperative Control Quandary Peak III Chaired by: T. SHIMA, Technion - Israel Institute of Technology, Haifa, Israel, and R. LIND, University of Florida, Gainesville, FL 1400 AIAA-2006-6453 UAV Coordination for Autonomous Target Tracking R. Wise and R. Rysdyk, University of Washington, Seattle, WA 1430 AIAA-2006-6454 Robust Decentralized Task Assignment for Cooperative UAVs M. Alighanbari and J. How, Massachusetts Institute of Technology, Cambridge, MA 1500 AIAA-2006-6455 A Modular Software Infrastructure for Distributed Control of Collaborating UAVs A. Ryan, X. Xiao, S. Rathinam, J. Tisdale, M. Zennaro, D. Caveney, R. Sengupta, and J. Hedrick, University of California, Berkeley, Berkeley, CA 1530 AIAA-2006-6456 UAV Cooperative Task Assignments for a SEAD Mission Using Genetic Algorithms M. Darrah, W. Niland and B. Stolarik, Institute for Scientific Research, Fairmont, WV; L. Walp, West Virginia University, Morgantown, WV 1600 AIAA-2006-6457 Quasi- Decentralized Task Assignment for Multiple UAV Coordination J. Ousingsawat, King Mongkut's Institute of Technology, Bangkok, Thailand 1630 AIAA-2006-6458 Optimal Decision Rules and Human Operator Models for UAV Operations P. Chandler, Air Force Research Laboratory, Wright-Patterson AFB, OH; A. Girard, Columbia University, New York, NY; and M. Pachter, Air Force Institute of Technology, Wright-Patterson AFB, OH 1700 AIAA-2006-6459 Concentration Gradient and Information Energy for Decentralized UAV Control W. Pisano, D. Lawrence, and K. Mohseni, University of Colorado at Boulder, Boulder, CO 1730 AIAA-2006-6460 Bayesian Forecasting in Multi- vehicle Search Operations L. Bertuccelli and J. How, Massachusetts Institute of Technology, Cambridge, MA Session 75- GNC-37 UAV Cooperative Control and Communication Gray's Peak III Chaired by: D. JEFFCOAT and H. PFISTER, U.S. Air Force Research Laboratory, Eglin AFB, FL 1400 AIAA-2006-6461 Cooperative Target Tracking for Autonomous UAVs in an Adversarial Environment U. Zengin and A. Dogan, University of Texas at Arlington, Arlington, TX 1430 AIAA-2006-6462 An Approach to Controlling Swarms of Unmanned Aerial Vehicles in Adversarial Situations J. Reimann and G. Vachtsevanos, Georgia Institute of Technology, Atlanta, GA; L. Tang and J. Ge, Impact Technologies, Rochester, NY 1500 AIAA-2006-6463 Maintaining a Linked Network Chain of Unmanned Aircraft Utilizing Decentralized Mobility Control C. Dixon and E. Frew, University of Colorado at Boulder, Boulder, CO 1530 AIAA-2006-6464 Phase Transitions for Controlled Mobility in Wireless Ad Hoc Networks C. Dixon, D. Henkel, T. Brown, and E. Frew, University of Colorado at Boulder, Boulder, CO 1600 AIAA-2006-6465 Networked UAV Command, Control and Communication J. Elston, E. Frew, and B. Argrow, University of Colorado at Boulder, Boulder, CO 1630 AIAA-2006-6466 Wireless Wide Area Networked System for Navigation, Communication and Tracking N. Coleman, K. Lam, and G. Papanagopoulos, U.S. Army Armament Research, Development and Engineering Center, Picatinny Arsenal, NJ; and C. Lin, American GNC Corporation, Simi Valley, CA 1700 AIAA-2006-6467 Vector Field Approach for Curved Path Following for Miniature Aerial Vehicles S. Griffiths, Brigham Young University, Provo, UT 1730 AIAA-2006-6468 Using Telemetry Data for Video Compression on Unmanned Air Vehicles A. Rodriguez, B. Ready and C. Taylor, Brigham Young University, Provo, UT Session 76- MST-11 Aerospace Modeling Techniques and Applications Castle Peak II Chaired by: J. KRUEP, Aerojet, Fairfax, VA 1400 AIAA-2006-6469 Agent- Based Modeling with Polygon Primitives for Aerospace Applications S. Goldfarb, V. Rao and R. D'Andrea, Cornell University, Ithaca, NY 1430 AIAA-2006-6471 A Simulation Benchmark for Integrated Fault Tolerant Flight Control Evaluation H. Smaili and J. Breeman, National Aerospace Laboratory NLR, Amsterdam, The Netherlands; T. Lombaerts and D. Joosten, Delft University of Technology, Delft, The Netherlands 1500 AIAA-2006-6472 How to Choose State Variables for Numerical Simulations of Aerospace Systems P. Gurfil and I. Klein, Technion-Israel Institute of Technology, Haifa, Israel 1530 AIAA-2006-6473 Parameter Based Fatigue Life Analysis, Influence of Training Data Selection to Analysis Performance J. Tikka, Patria Aviation, Halli, Finland; J. Ahola and M. Hiirsalmi, Technical Research Centre of Finland, Espoo, Finland Session 78- MST-13 Modeling and Simulation of Unconventional Vehicles and Vehicle Subsystems Castle Peak III Chaired by: B. HILDRETH, Science Applications International Corporation, Lexington Park, MD 1400 AIAA-2006-6480 Dynamic Coupling of the KC- 135 Tanker and Boom for Modeling and Simulation A. Smith, Air Force Research Laboratory, Wright-Patterson AFB, OH; and D. Kunz, Air Force Institute of Technology, Wright-Patterson AFB, OH 1430 AIAA-2006-6481 A Vision Based Navigation Among Multiple Flocking Robots: Modeling And Simulation B. Eikenberry, O. Yakimenko and M. Romano, Naval Postgraduate School, Monterey, CA 1500 AIAA-2006-6482 Simulation of an Ornithopter with Active Flow Control and Aeroelestic Energy Harvesting T. Apker, University of Notre Dame, Notre Dame, IN 1530 AIAA-2006-6483 Dynamic Stability Study of a Conceptual Fluidic Thrust- Vectored Aerial Tail- sitter F. Saghafi and A. Banazadeh, Sharif University of Technology, Tehran, Iran 1600 AIAA-2006-6808 Flexible Uses of Simulation Tools in an Academic Environment B. Lawrence, G. Padfield and P. Perfect, University of Liverpool, Liverpool, Great Britain Session 79-MST-14 1400 - 1730 Panel Session: MSTC Motion Working Group Castle Peak I Guest Speaker: Dr. Barbara Sweet, NASA Ames Research Center Topics: Visual Cueing for Vehicular Control Discussions on human visual systems, human visual sensitivities, and simulation cueing interactions in ground-based flight simulators. Motion Agenda Update: Dr. Ruud Hosman, AMS Consult Topics: Progress in developing lessons learned Updates and summary will be presented, which cover human sensory characteristics, cueing integration, human operator behavior, and standard and regulations. Moderator/s: W. Chung 1830 - 2030 Lakeside BBQ Dinner Decatur Field