Emulation and Analysis of Micro-accelerometer Based on Dynamics Model of Projectile Vehicle with High Dynamic
In this paper, from the point of view of Gyro-Free Strap-down Micro-Inertial Measurement System(GFSMIMS)and in terms of the characteristics of vehicle with high dynamic, the projectile launch dynamics problems involved in the theory of gyro-free projectile attitude measurement system are discussed; the launch and flight principle of controllable projectile system is analyzed, a launch and flight dynamics model of controllable projectile is proposed, and the projectile dynamics equations in boost phase and power-off phase are presented; in the whole trajectory flight circumstance of a model projectile, the launch and flight dynamics characteristics of controllable projectile and the output of all micro-accelerometers are simulated, the emulation results are given, and the corresponding analysis and conclusion are proposed.
Trajectory dynamics Micro-accelerometer Emulation and Analysis
LI Qin ZHANG Wendong FENG Pan
Key Laboratory of Instrumentation Science & Dynamic Measurement (North University of China), Ministry of Education National Key Laboratory for Electronic Measurement Technology Department of Electronic Science and technology, North university of China, Ta
国际会议
北京
英文
2007-08-05(万方平台首次上网日期,不代表论文的发表时间)