测量噪声下的高超声速飞行器组合观测鲁棒控制

Translated title of the contribution: Robust Control of Hypersonic Flight Vehicle Based on Combined State Observation Under Measurement Noises

Rui Zhang, Shihua Li, Zhenyan Wei, Bin Xu

Research output: Contribution to journalArticlepeer-review

Abstract

In response to the poor performance and even instability of the control system caused by existed external disturbances and measurement noises, a robust control strategy based on state observation is proposed. Considering the unstable controller caused by using inaccurate system states under disturbances and noises, the special combination of extended state observer (ESO) and adaptive Kalman filter (AKF) is proposed to accurately estimate the system states which are contaminated by disturbances and noises that with unknown statistical properties. The AKF is used to offset noises and to provide the ESO with noiseless state estimation, while the ESO continuously provides the estimation of wind disturbances for the AKF. To achieve good tracking performance, the linear quadratic Gaussian control using the states estimation of observer is designed for HFV. Simulations are implemented to verify that robust tracking is obtained under the proposed method.

Translated title of the contributionRobust Control of Hypersonic Flight Vehicle Based on Combined State Observation Under Measurement Noises
Original languageChinese (Traditional)
Pages (from-to)203-211
Number of pages9
JournalYuhang Xuebao/Journal of Astronautics
Volume45
Issue number2
DOIs
StatePublished - Feb 2024

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