Attitude control of launch vehicle is to control the attitude of launch vehicle, bring about the flight prosedure, and flight steadily under various disturbed circumstances. Combined with the background of launch vehicle engineering technology in China, the dynamic modeling, linearization analysis of small deviations and frequency domain design method of attitude control system are described.

Hao pan, graduated from the Academy of mathematics and Systems Science Research Institute in 2011, now working as a senior engineer in the 12-th research laboratory of the first research institute of China Aerospace Science and Technology Corporation, is mainly engaged in the design of attitude control system of manned space launch vehicle.