Estimates of key airframe parameters, obtained from in-flight parameter identification, are used to adjust flight control system parameters to meet performance objective; by combining equations-of-motion approach with analog steepest descent, practical parameter identification scheme is obtained which accounts for all inputs to aircraft, and yet is simply mechanized by analog hardware.
Parameter identification -- Key to second-generation adaptive flight control
Sperry Rand Eng Rev
Sperry Rand Engineering Review ; 21 , n 2
1968
8 pages
Article (Journal)
English
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