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On the Attitude Stabilization of a Rigid Spacecraft Using Two Control Torques
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On the Attitude Stabilization of a Rigid Spacecraft Using Two Control Torques
On the Attitude Stabilization of a Rigid Spacecraft Using Two Control Torques
HK
Hariharan Krishnan
Hariharan Krishnan
HM
Harris McClamroch
Harris McClamroch
MR
Mahmut Reyhanoglu
Mahmut Reyhanoglu
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1 June 1992
conference paper
conference paper
Published by
Institute of Electrical and Electronics Engineers (IEEE)
https://doi.org/10.23919/acc.1992.4792472
Abstract
No abstract available
Cited by 38 articles