一种自适应控制增稳方案的实时仿真研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (6): 269-275.

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SIMULATION STUDY ON A SCHEME OF ADAPTIVE CONTROL STABILITY AUGMENTATION

Zhang Ning, Xiao Shunda

Northwestern Polytechnical University

Received:1988-01-03 Revised:1900-01-01 Online:1990-06-25 Published:1990-06-25

Abstract

Abstract: In this paper a real time hybrid simulation research on a PACAS (Parameter Adaptive Command Augmentation System) scheme is presented. It includes both software design, programming and system performence analysis based on simulation. It shows that the design of system software is feasible with high computing accuracy, stability and reliability, and the PACAS scheme, which has strong adaptation ability, makes the flying quality reqirements described in MIL-F-8785B and MIL-F-9490C be well satisfied.

Key words: adaptive control, stability lugmentation system, parameter identification Kalman filtering

Zhang Ning;Xiao Shunda. SIMULATION STUDY ON A SCHEME OF ADAPTIVE CONTROL STABILITY AUGMENTATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(6): 269-275.

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