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GYRO BIAS ON-ORBIT CALIBRATION FOR MICRO SATELLITES 被引量:1
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作者 郁丰 刘建业 熊智 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2007年第4期300-304,共5页
According to gyro application in micro-satellites, a new gyro bias real-time on-orbit calibration technology is presented and it is independent of any other sensors. The approach relies on gyro on-orbit measurements r... According to gyro application in micro-satellites, a new gyro bias real-time on-orbit calibration technology is presented and it is independent of any other sensors. The approach relies on gyro on-orbit measurements restricted by satellite attitude dynamics and estimates the gyro bias generated when the gyro is electrified. Observability of the calibration model is analyzed and applicable conditions of the technology are derived. Simulation results indicate that the calibration algorithm is accurate and robust at gyro sampling rate, and its convergence speed is fast. Within the given attitude dynamics model error, the convergence time is less than 100 s and the convergence accuracy is about 1.0 (°)/h. Calibration performance can meet requirements of spacecraft operations. 展开更多
关键词 on-orbit calibration gyro bias Kalman filter micro satellite
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