J-GLOBAL ID:200904005767441127  Research Project code:9800016544 Update date:Jan. 19, 2004

Study on the testing method of the movement of posture control system of missile

Study period:1990 - 2002
Organization (1):
Investigating Researcher (8):
Research overview:
On the posture control equipment, which is amounted on missile or scientific satellite, study on the testing method of the amounted sensor and practical movement of hardware and software is preformed. As a simulation of the movement in cosmic space, active closing loop test using the motion table with 3 wheels and static closing loop test only using the sensor electric circuit are performed. In addition, in order to measure the effect of disturbance occurring from posture control actuators, the disturbance occurring from the momentum wheel with three components dynamometer and mechanical gyro was measured, and the evaluation of the effect to the posture control of satellite was performed.
Keywords (5):
artificial satellite ,  sensor ,  performance test ,  attitude control ,  simulation
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

Return to Previous Page