Next generation entry guidance - Onboard trajectory generation for unpowered drop tests
Author:
Affiliation:
1. Charles Stark Draper Lab., Inc., Cambridge, MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3960
Reference6 articles.
1. (Examplefromconstant flight pathangle) - 4 - 2 0 2 4 6
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1. On-line guidance with trajectory constraints for terminal area energy management of re-entry vehicles;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-05-16
2. Integrated Adaptive Guidance and Control for Re-Entry Vehicles with Flight Test Results;Journal of Guidance, Control, and Dynamics;2004-11
3. Fuzzy Logic Trajectory Design and Guidance for Terminal Area Energy Management;Journal of Spacecraft and Rockets;2004-05
4. On-Line Trajectory Command Reshaping for Reusable Launch Vehicles;AIAA Guidance, Navigation, and Control Conference and Exhibit;2003-06-22
5. On-Board Generation of Three-Dimensional Constrained Entry Trajectories;AIAA Guidance, Navigation, and Control Conference and Exhibit;2002-06-25
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