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The Method of Interference Compensation and Measurement for the Attitude Control System
Pages: 1-14
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Attitude control system Interference Measurement Compensation.;
Abstract: According to the complete compensation conditions of the system, this paper is to prove that the pitch and yaw channel of the missile body attitude motion can’t compensate completely the interferences, but can do it for the roll channel. This paper relates the complete compensation method for the pitch channel, and puts forward an idea of overcoming the in fluences of the dynamic characteristics of servo system for the compensation. We also discuss the inter ference measuring method using the meter of attack angle, angular accelermeter and observer, as well the method of using feedback to realize the static inter ference compensation.
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