Selected stability and control derivatives from the first Space Shuttle entry-Reference-Cited by-同舟云学术

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Selected stability and control derivatives from the first Space Shuttle entry

Published:1981-08-17 Issue: Volume: Page:
ISSN:
Container-title:1st Flight Test Conference
language:
Short-container-title:

Author:

ILIFF K.¹,MAINE R.¹,COOKE D.²

Affiliation:

1. NASA, Flight Research Center, Edwards, CA

2. NASA,Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1981-2451

Reference11 articles.

1. Evaluation of the Space Shuttle Orbiter and Carrier Aircraft NASA Approach and Landing Test. AFFTC-TR-78-17, May 1978. 2. Cooke, Douglas R . : Subsonic Stabil

2. ity and Control Flight Test Results of the space Shuttle (Tail Cone Off). AIAA Paper 80-1604, Aug. 1980. Aerodynamic Design Data Book, Orbiter

Cited by 4 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. Parameter estimation for flight vehicles;Journal of Guidance, Control, and Dynamics;1989-09

2. Aircraft parameter estimation;25th AIAA Aerospace Sciences Meeting;1987-03-24

3. Uses of parameter estimation in flight test;Journal of Aircraft;1983-12

4. Space Shuttle entry aerodynamic comparisons of flight 1 with preflight predictions;Journal of Spacecraft and Rockets;1983-01

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