＂Tian Tuo 1＂ （TT-1） nano-satellite is the first single-board nano-satellite that was suc- cessfully launched in China. The main objective of TT-1 is technology demonstration and scientific measurements. The satell...＂Tian Tuo 1＂ （TT-1） nano-satellite is the first single-board nano-satellite that was suc- cessfully launched in China. The main objective of TT-1 is technology demonstration and scientific measurements. The satellite carries out the significant exploration of single-board architecture fea- sibility validation, and it is tailored to the low-cost philosophy by adopting numerous commercial- off-the-shelf （COTS） components. The satellite is featured with three-axis stabilization control capability. A pitch bias momentum wheel and three magnetic coils are adopted as control actuators. The sun sensors, magnetometers and a three-axis gyro are employed as the measurement sensors. The quaternion estimator （QUEST） and unscented Kalman filter （UKF） method are adopted for the nano-satellite attitude determination. On-orbit data received by ground station is conducted to analysis the performance of attitude determination and control system （ADCS）. The results show that the design of ADCS for TT-1 is suitable, robust and feasible.展开更多
文摘＂Tian Tuo 1＂ （TT-1） nano-satellite is the first single-board nano-satellite that was suc- cessfully launched in China. The main objective of TT-1 is technology demonstration and scientific measurements. The satellite carries out the significant exploration of single-board architecture fea- sibility validation, and it is tailored to the low-cost philosophy by adopting numerous commercial- off-the-shelf （COTS） components. The satellite is featured with three-axis stabilization control capability. A pitch bias momentum wheel and three magnetic coils are adopted as control actuators. The sun sensors, magnetometers and a three-axis gyro are employed as the measurement sensors. The quaternion estimator （QUEST） and unscented Kalman filter （UKF） method are adopted for the nano-satellite attitude determination. On-orbit data received by ground station is conducted to analysis the performance of attitude determination and control system （ADCS）. The results show that the design of ADCS for TT-1 is suitable, robust and feasible.
