摘要
为了评估单向多普勒测速动态测量精度,构建了一种基于卫星信道模拟器的测速精度评估系统,通过在卫星信道模拟器装订卫星飞行轨迹,利用卫星信道模拟器对上行信号加入传播时延、多普勒频率,对卫星在轨飞行状态下的单向多普勒测速进行场景仿真,并对场景仿真获取的测速数据进行O-C残差序列分析,得到动态测量条件下的测速精度。给出了O-C残差序列的计算方法,分析了单向多普勒测速体制下时钟偏差对测速结果的影响,并给出了一种简单的时钟误差修正方法。
A range rate measurement accuracy evaluation system was constructed based on satellite channel simulator to evaluate the dynamic measurement accuracy of one-way Doppler range rate measurement.Scenario simulation was performed for one-way Doppler range rate measurement of an in-flight satellite by binding satellite flight trajectory in a satellite channel simulator and using satellite channel simulator to add propagation delay and Doppler frequency to the uplink signal.O-C residual sequence analysis was done on the range rate measurement data obtained from the scenario simulation to get range rate measurement accuracy under dynamic measurement conditions.O-C residual sequence calculation method is given and the impact of clock offset on range rate measurement results in one-way Doppler range rate measurement system was analyzed.A simplified clock error correction method is presented.
出处
《飞行器测控学报》
CSCD
2015年第4期357-361,共5页
Journal of Spacecraft TT&C Technology
关键词
测速精度评估
卫星信道模拟器
O-C计算
时钟偏差
时钟误差修正
单向多普勒测速
evaluation of range rate measurement accuracy
satellite channel simulator
O-C calculation
clock offset
clock error correction
one-way Doppler range rate measurement