摘要
从运载火箭的核心仪表陀螺加速度计对输出装置的技术要求出发，讨论了陀螺加速度计输出装置设计中的技术问题，提出了一种新型的小型化高速高精度动态测角系统方案。另外还探讨了输出装置精度的测试问题，提出了具有实用意义的测试方法。
The technical requirements of output system of Pendulous Integrating Gyro Accelerometer(PIGA) are discussed. A practical high speed dynamic angle measuring system has been designed for PIGA output signal detection. The engineering problems in instrument testing have been solved, and some testing methods have been presented.
出处
《导弹与航天运载技术》
1995年第3期36-43,共8页
Missiles and Space Vehicles
关键词
加速度计
陀螺仪
惯性导航
精度分析
Accelerometer, Gyroscope, Inertial Navigation, Accuracy analysis.
