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Integrated guidance and control design method based on finite-time state observer 被引量:1
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作者 MA Ping ZHANG Denghui +1 位作者 WANG Songyan CHAO Tao 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2018年第6期1251-1262,共12页
A composited integrated guidance and control(IGC) algorithm is presented to tackle the problem of the IGC design in the dive phase for the bank-to-turn(BTT) vehicle with the inaccuracy information of the line-of-sight... A composited integrated guidance and control(IGC) algorithm is presented to tackle the problem of the IGC design in the dive phase for the bank-to-turn(BTT) vehicle with the inaccuracy information of the line-of-sight(LOS) rate. For the sake of theoretical derivation, an IGC model in the pitch plane is established. The high-order finite-time state observer(FTSO), with the LOS angle as the single input, is employed to reconstruct the states of the system online. Besides, a composited IGC algorithm is presented via the fusion of back-stepping and dynamic inverse. Compared with the traditional IGC algorithm, the proposed composited IGC method can attenuate effectively the design conservation of the flight control system, while the LOS rate is mixed with noise. Extensive experiments have been performed to demonstrate that the proposed approach is globally finite-time stable and strongly robust against parameter uncertainty. 展开更多
关键词 integrated guidance and control(IGC) finite-time state observer(FTSO) back-to-turn(BTT) vehicle composited control
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