Adaptive two-axis acceleration control and roll stabilization of air-to-air missile is analyzed and simulated; adaptive principle consists of relocating open loop zeros to region of S-plane having prescribed damping and frequency characteristics, and cyclically increasing forward loop gain to drive control surface actuator poles across imaginary axis at fixed frequency; factors to consider in application and mechanization of control system are presented.
Design, analysis and simulation of self-adaptive acceleration flight control system
AIAA -- Simulation Aerospace Flight Conference -- Tech Papers
AIAA -- Simulation for Aerospace Flight Conference ; 1963 Control
1963
9 pages
Conference paper
English
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