Influence estimation of reaction wheel position errors of spacecraft attitude control system on its attitude control accuracy

1Khoroshylov, EV, 1Khoroshylov, SV
1Institute of Technical Mechanics of the National Academy of Science of Ukraine and the State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2005, 11 ;(Supplement1):005-011
Publication Language: Russian
Abstract: 
Different reaction wheel installation schemes of the spacecraft attitude control system are considered. The influence of the reaction wheel position errors on the spacecraft attitude control accuracy is investigated. The relations which allow one to evaluate the influence of these errors on the accuracy characteristic of the attitude control system are derived. Our results of numerical evaluations for possible operational cases of the reaction wheel installation schemes under consideration are presented.
References: 

1. Belousov K. G., Melanchenko A. G., Saltykov Yu. D. Optimization of the spatial configuration of flywheels in satellite attitude control problems. In: Small satellites. New technologies, miniaturization. Areas of the effective application in XXI century: II International. Conference and Exhibition. 1—6 (Korolev, 2000) [in Russian].
2. Raushenbakh B. V., Tokar E. N. Orientation control of spacecraft, 598 p. (Nauka, Moscow, 1974) [in Russian].