4.7 Article

Hybrid Disturbance Observer-Based Anti-Disturbance Composite Control With Applications to Mars Landing Mission

Journal

IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS
Volume 51, Issue 5, Pages 2885-2893

Publisher

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TSMC.2019.2917528

Keywords

Anti-disturbance composite control; hybrid disturbance observer; Mars landing powered descent phase; multiple sources of disturbances

Funding

  1. National Natural Science Foundation of China [61627810, 61320106010, 61633003, 61603021, 61833013]
  2. Program for Changjiang Scholars and Innovative Research Team [IRT16R03]
  3. Foundation of Science and Technology on Aircraft Control Laboratory [WDZC2019601A104]

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This paper proposes a hybrid anti-disturbance composite control scheme, employing a hybrid disturbance observer and H∞ technique to address external disturbances and actuator discrete dynamics, ensuring precise execution of the entire hybrid system, with stability analysis of the continuous-discrete control system.
In this paper, a hybrid anti-disturbance composite control scheme is presented to address the problem subject to systems remarkably affected by external disturbances and discrete dynamics of actuators. By explicitly considering the hybrid feature resulting from discrete actuation signals acted on a continuous system, the hybrid disturbance observer is designed to estimate the effect of external disturbance. Meanwhile, H-infinity technique is used to mitigate the effect of continuous command executing error caused by discontinuous operation, which cannot be modeled in priori. Within the proposed composite control scheme, the combination of the disturbance estimation information and the H-infinity technique enables the entire hybrid system precisely performing. The stability of the whole continuous-discrete control system is analyzed. Finally, based on the Mars lander dynamics, comparative simulation studies illustrate that the developed control scheme can preserve a satisfactory level of performance, even in the presence of external disturbances and actuator quantization errors.

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