Two distinct methods to effect control action are described and two arrangements illustrated; factors which affect dynamic characteristics of aircraft can be classified as environmental, geometrical, flight-mode, and internal factors; direct method of providing variable-parameter controller and its disadvantages; requirements for self-adaptive system and description of system developed by Aviation Div of Smiths Industries Ltd; method of obtaining autostabilizer parameters by direct measurement of aircraft characteristics and operation of system; effect of finite snr; applications.
Self-adaptive control of aircraft
Flight
Flight International ; 91 , n 3023
1967
Article (Journal)
English
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