Minimum control power for VTOL aircraft stability augmentation
Author:
Affiliation:
1. Purdue University, Lafayette, Ind.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44151
Reference21 articles.
1. Study of VTOL Control Requirements During Hovering and Low‐Speed Flight Under IFR Conditions
2. Sadoff, M. "A Study of a Pilot's Ability to Control During Simulated Stability Augmentation System Failures,'' TN D-1552, Nov. 1962, NASA.
3. Status of vstol research and development in the united states
Cited by 3 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. VTOL aircraft control power costs;3rd Aircraft Design and Operations Meeting;1971-07-12
2. Comment on "Minimum Control Power for VTOL Aircraft Stability Augmentation";Journal of Aircraft;1971-04
3. Reply by Author to H. C. Curtiss Jr.;Journal of Aircraft;1971-04
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