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International Journal of Systems Science Volume 53, 2022 - Issue 1

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High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation

Guangren Duana Center for Control Science and Technology, Southern University of Science and Technology, Shenzhen, People's Republic of China;b Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, People's Republic of ChinaCorrespondence[email protected]
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https://orcid.org/0000-0002-8169-2218 View further author information

Pages 54-73 | Received 24 Jan 2021, Accepted 28 May 2021, Published online: 19 Jun 2021

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https://doi.org/10.1080/00207721.2021.1937750
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Figure 1. Coordinate system transformation.

Figure 2. Simulation results for attitude stabilisation, Case A1.

Figure 3. Simulation results for attitude stabilisation, Case A2.

Figure 4. Simulation results for turning elimination, Case B1.

Figure 5. Simulation results for turning elimination, Case B2.

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