インパルス制御源を用いたスピン飛しょう体の姿勢制御 : 第1報, 離散時間のスライディングモード制御系の設計

概要

論文の詳細を見る
Sliding mode control is applied to the attitude control of a spinning vehicle by the combination of one-shot thrusters that generate lateral thrust with a pulse width of less than 1 ms. This thruster system has several advantages such as small control delay and low cost, and can be used in high altitude, low dynamic pressure and hyper sonic enviroments. We adopt the regulator scheme to reject disturbances of precession for the LUNAR-A penetrator of a lunar probe. The Control system is designed for discrete time computer control and thruster consumption has been reduced by using the method of linear quadratic optimal control applied to the design of switching hyperplanes. This reduction results in a lower total weight of the vehicle.
一般社団法人日本機械学会の論文
1998-05-25