The results show that gravity disturbance vector is a major error source for high accuracy inertial navigation system.
结果表明，不确定的重力扰动向量是高精度惯导系统的一个重要误差源。
The law on coupling effect and gravity load impacting control error of the target simulator was studied.
对耦合效应及重力负载影响目标模拟器控制误差的规律进行了对比研究。
A detailed analysis is made on the error result from factors mentioned above when using center of gravity method.
通过实验对重心法运用于这类系统将产生的误差作了较为详尽的分析。
应用推荐