Controlling Chaotic Attitude Motion of Spacecraft by the Input-Output Linearization

DOI<link itemprop=identifier href="https://doi.org/10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y" /><701::AID-ZAMM701>3.0.CO;2-Y 10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-YzbMath0970.70019OpenAlexW2003118779MaRDI QIDQ4521676

Yan-zhu Liu, Li Qun Chen

Publication date: 21 December 2000

Full work available at URL: https://doi.org/10.1002/1521-4001(200010)80:10<701::aid-zamm701>3.0.co;2-y

zbMATH Keywords

nonlinear feedback controlgravitational fieldinput-output linearizationelliptic orbitinternal dampingair dragcontrol of chaotic oscillationsattitude motion of spacecraft

Mathematics Subject Classification ID

Transition to stochasticity (chaotic behavior) for nonlinear problems in mechanics (70K55) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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Control of chaos and its relevancy to spacecraft steering

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