公开(公告)号：US3838834A

公开(公告)日：1974-10-01

申请号：US31936672

申请日：1972-12-29

Applicant: RCA CORP

Inventor： MICHAELIS T

IPC: B64G1/28 ,  B64G1/32 ,  B64G1/36 ,  B64G1/00

CPC classification number: B64G1/36 ,  B64G1/283 ,  B64G1/288 ,  B64G1/32 ,  B64G1/361 ,  B64G1/363 ,  B64G1/365 ,  Y10S136/292

Abstract: A satellite is compensated for torques caused by solar pressure on a solar panel extending from the satellite by an air core coil energized to develop a magnetic torque in opposition to the solar pressure torque. The coil is disposed generally in the periphery of the solar panel mounted externally to the satellite. The energizing current is fixed or varied by ground command or automatically in a closed loop system to compensate for variations in the earth''s magnetic field.

Abstract translation: 卫星补偿由太阳能电池板上的太阳能压力引起的扭矩，该太阳能电池板由空气芯线圈从卫星延伸，通电，以产生与太阳能压力扭矩相反的磁力矩。 线圈通常设置在安装在卫星外部的太阳能电池板的周边。 励磁电流由地面指令固定或变化，或在闭环系统中自动进行，以补偿地球磁场的变化。