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Event-Triggered Attitude Tracking for Rigid Spacecraft

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Event-Triggered Active Disturbance Rejection Control

Part of the book series: Studies in Systems, Decision and Control ((SSDC,volume 356))

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Abstract

In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1,2,3,4,5].

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Authors and Affiliations

  1. School of Automation, Beijing Institute of Technology, Beijing, China

    Dawei Shi, Yuan Huang & Junzheng Wang

  2. Department of Electronic and Computer Engineering, Hong Kong University of Science and Technology, Hong Kong, Hong Kong

    Ling Shi

Authors
  1. Dawei Shi
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  2. Yuan Huang
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  3. Junzheng Wang
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  4. Ling Shi
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Corresponding author

Correspondence to Dawei Shi .

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Shi, D., Huang, Y., Wang, J., Shi, L. (2021). Event-Triggered Attitude Tracking for Rigid Spacecraft. In: Event-Triggered Active Disturbance Rejection Control. Studies in Systems, Decision and Control, vol 356. Springer, Singapore. https://doi.org/10.1007/978-981-16-0293-1_8

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