An algorithm for the active stabilization of a spacecraft with viscoelastic elements under conditions of uncertainty

✍ Scribed by M.S. Yefremov; A.Ye. Polyakov; V.V. Strygin

• Publisher: Elsevier Science
• Year: 2006
• Tongue: English
• Weight: 300 KB
• Volume: 70
• Category: Article
• ISSN: 0021-8928
• DOI: 10.1016/j.jappmathmech.2006.11.007

✦ Synopsis

An algorithm for stabilizing the angular position of a spacecraft with dynamic elastic elements possessing dissipative properties is proposed, based on bang-bang feedback with delay. The control is achieved under conditions of uncertainty. The accuracy of the equation is demonstrated by a numerical example.