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An Evaluation on the Limit cycle Analysis Methods using the Hardware in the Loop Simulation  

Jeon, Sang-Woon (한국항공우주연구원 나로호체계종합팀)
Publication Information
Aerospace Engineering and Technology / v.11, no.1, 2012 , pp. 145-157 More about this Journal
Abstract
The novel limit cycle analysis of the attitude control system using jet thrusters was presented based on a phase plane method by paper. It was shown in the software simulation results that the analysed results of the limit cycle was more accurate than those of the Haloulakos' method. But it was not verified in the real system. The proposed method is verified in the reaction control system for KSLV-I via an real time hardware in the loop simulation. It can be shown in this test that analyzed result of the limit cycle is very accurate.
Keywords
reaction control system; limit cycle; hardware in the loop simulation; phase plane;
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