Suboptimal LQR-based spacecraft full motion control: Theory and experimentation
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- 作者：Leone Guarnacciab ; 1 ; leone.guarnaccia@gmail.com" class="auth_mail" title="E-mail the corresponding authorAuthor Vitae ; Riccardo Bevilacquaa ; bevilr@ufl.edu" class="auth_mail" title="E-mail the corresponding authorAuthor Vitae ; Stefano P. Pastorellib ; 2 ; stefano.pastorelli@polito.it" class="auth_mail" title="E-mail the corresponding authorAuthor Vitae
- 关键词：ADAMUS ; Advanced Autonomous Multiple Spacecraft ; APF ; artificial potential function ; AS ; attitude stage ; BP ; balancing platform ; CPU ; central processing unit ; DARPA ; Defense Advanced Research Projects Agency ; DCM ; direction cosine matrix ; EKF ; extended Kalman filter ; GDC ; guidance dynamics corporation ; IBPS ; intelligent battery and power system ; IPOPT ; interior point optimizer ; KKT ; Karush&ndash ; Kuhn&ndash ; Tucker ; LGR ; Legendre Gauss Radau ; LKF ; linear Kalman filter ; LQE ; linear quadratic estima
- 刊名：Acta Astronautica
- 出版年：2016
- 出版时间：May-June 2016
- 年：2016
- 卷：122
- 期：Complete
- 页码：114-136
- 全文大小：4358 K
文摘
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Full spacecraft motion control based on Linear Quadratic Regulator.
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Full experimental validation in a laboratory environment.
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Full cost comparison versus a numerical optimal control solver.