Optimal Guidance for the Space Shuttle Transition

Author:

STENGEL ROBERT F.1

Affiliation:

1. The Analytic Sciences Corporation, Reading, Mass.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Design and Evaluation of an Acceleration Guidance Algorithm for Entry;Journal of Spacecraft and Rockets;2004-11

2. Landing Footprint Computation for Entry Vehicles;AIAA Guidance, Navigation, and Control Conference and Exhibit;2004-06-22

3. Design and Evaluation of an Acceleration Guidance Algorithm for Entry;AIAA Guidance, Navigation, and Control Conference and Exhibit;2003-06-22

4. Performance of Evolved Acceleration Guidance Logic for Entry (EAGLE);AIAA Guidance, Navigation, and Control Conference and Exhibit;2002-06-25

5. Reduced-Order Entry Trajectory Planning for Acceleration Guidance;Journal of Guidance, Control, and Dynamics;2002-03

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