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Distributed fixed-time output-feedback attitude consensus control for multiple spacecraft with input saturation
Received date: 2022-05-18
Revised date: 2022-06-09
Accepted date: 2022-07-04
Online published: 2022-07-08
Supported by
National Natural Science Foundation of China(61873312)
This paper studies the distributed fixed-time output-feedback attitude consensus control problem of multiple spacecraft with input saturation under directed graph. First， only a part of the spacecrafts can obtain the attitude and angular velocity state information of the leader. A fixed-time observer of leader’s attitude is designed to estimate leader’s attitude. Then， for the issue that spacecrafts being unable to measure their own ungular velocity， this paper proposes a fixed-time state observer to estimate the angular velocity of spacecraft in a fixed time. Based on the estimated leader’s attitude and spacecraft angular velocity， a fixed-time attitude tracking controller is proposed， and the fixed-time stability of the spacecraft attitude system is proved rigorously. Finally， some simulations are conducted， and simulation results verify the effectiveness of the proposed control scheme.
Chuang XU , Baolin WU . Distributed fixed-time output-feedback attitude consensus control for multiple spacecraft with input saturation[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(10) : 327465 -327465 . DOI: 10.7527/S1000-6893.2022.27465
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