NONLINEAR DYNAMIC RESEARCH OF THE SPACECRAFT ROBUST FAULT TOLERANT CONTROL SYSTEMS
Ye.I. Somov*,†, A.G. Kozlov‡, V.A. Rayevsky‡,
G.P. Anshakov†, Yu.G. Antonov§
* Research Institute of Mechanical Systems Reliability
(NII PNMS), Samara State Technical University
244 Molodogvargeyeskaya Str. Samara 443100 Russia
somov@icc.ru pnms@sstu.edu.ru
† Stability and Nonlinear Dynamics Research Center,
Mechanical Engineering Research Institute (IMash),
the Russian Academy of Sciences (RAS)
5 Dm. Ul’yanov Str. Moscow 117333 Russia
‡ Research & Production Association “Applied Mechanics”
(NPO PM), the Russian Space Agency (RKA)
52 Lenin Str. Krasnoyarsk-26 660026 Russia
§ State Research & Production Rocket - Space Center
“TsSKB-Progress”, the Russian Space Agency (RKA)
18 Pskovskaya Str. Samara 443009 Russia
New results on methods and software for nonlinear dynamic research and design of robust gyromoment fault tolerant control systems by the information spacecraft (remote sensing, communication, navigation and geodesic) developed by the leading Russian State Space Research and Production Associations (RPAs) --- the TsSKB-Progress and the NPO PM, are presented.
Keywords: spacecraft, attitude control system, fault tolerance, nonlinear dynamics
Session slot T-Mo-A06: Nonlinear, Robust and Fault Tolerant Aerospace Control S/Area code 8a : Aerospace
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