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29744458500
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An Aerobot For Global In Situ Exploration of Titan
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29344454952
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A Design Comparison of Atmospheric Flight Vehicles for the Exploration of Titan
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AIAA 2005-6235, San Francisco, California, August
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AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Gasbarre, J.F.1
Wright, H.S.2
Lewis, M.J.3
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3
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37249003698
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Dynamics and Control of a Herd of Sondes Guided by a Blimp on Titan
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Maui, Hawaii, February
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Robotic Airships for Exploration of Planetary Bodies with an Atmosphere: Autonomy Challenges
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Towards a Substantially Autonomous Aerobot for Exploration of Titan
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Design of a Missile Autopilot using Adaptive Nonlinear Dynamic Inversion
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Shell, W.M.2
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9
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Nonlinear Control Law with Application to High Angle-of-Attack Flight
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Flight Control Design Using Non-linear Inverse Dynamics
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Stability and Robustness Analysis of the AURORA Airship Control System using Dynamic Inversion
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29344459608
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Nonlinear Inversion Control for a Ducted Fan UAV
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AIAA 2005-6231, San Francisco, California, August
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Spaulding, C. M., Mansur, M. H., Tischler, M. B., Hess, R A., Franklin, J. A., "Nonlinear Inversion Control for a Ducted Fan UAV," AIAA 2005-6231, AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, California, August 2005.
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AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Spaulding, C.M.1
Mansur, M.H.2
Tischler, M.B.3
Hess, R.A.4
Franklin, J.A.5
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15
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0033721908
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Robust Flight Control Design with Handling Qualities Constraints Using Scheduled Linear Dynamic Inversion and Loop-Shaping
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0037284889
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Reentry Flight Controller Design Using Nonlinear Dynamic Inversion
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Da Costa, R.R.1
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17
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37249029811
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Dynamics, Design Study and Dynamic Inversion Control of a Nonlinear Autonomous Airship for the Exploration of Titan,
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Masters Thesis, Department of Mechanical and Aeronautical Engineering, University of California, Davis, CA
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Acosta, D. M., "Dynamics, Design Study and Dynamic Inversion Control of a Nonlinear Autonomous Airship for the Exploration of Titan," Masters Thesis, Department of Mechanical and Aeronautical Engineering, University of California, Davis, CA, 2006.
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Acosta, D.M.1
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18
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29744434659
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Six-Degree-of-Freedom Dynamic Airship Model in ADAMS,
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Masters Thesis, Department of Mechanical and Aeronautical Engineering, University of California, Davis, CA
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