Need for systems applied to commercial aircraft, drone and research vehicles, manned space craft, and recoverable missile boosters, is shown; automatic landing problems and limitations of exponential flare and path program systems; concept of 2-condition terminal flare controller, using altitude and altitude rate predictor; real time synthesis procedure provides direct design method for servo problems of terminal control type.
Automatic flare systems for aircraft, missiles, and space vehicles
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1958 Landing
1958
18 pages
Aufsatz (Konferenz)
Englisch
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