WEI Dong, ZHAO Zhi-shu, LI Ying-hong. Design of high precision inertial platform for aircraft based on liquid floated gyro[J]. 2014, 33(10): 97-99+114.
WEI Dong, ZHAO Zhi-shu, LI Ying-hong. Design of high precision inertial platform for aircraft based on liquid floated gyro[J]. 2014, 33(10): 97-99+114. DOI: 10.13873/J.1000-9787(2014)10-0097-03.
基于液浮陀螺的飞行器用的高精度惯性平台设计
摘要
设计了平台应用于飞行器轨迹的背景
研究了平台结构特点
从平台系统模型的角度分析了高精度三轴惯性稳定平台的工作原理;基于飞行器轨迹平台的特点
设计了一种新型的陀螺安装方式
利用直接驱动具有高精度、高速度、机械结构简单、可靠等优点
理论分析证明了此种安装方式的可行性和优越性
推导了系统的传递函数
且就偏心距和陀螺仪漂移的影响进行了仿真分析。
Abstract
Design background of platform applied in aircraft trajectory
research characteristics of platform structure
working principle of high precision three axis inertial stabilized platform is analyzed from the perspective of platform of system model;based on characteristics of aircraft trajectory platform
design installation mode of a new type of gyro
using advantages of direct drive has high precision
high speed
simple mechanical structure
reliable
theoretical analysis proves feasibility and superiority of this kind of installation mode
derive transmission function of system
and effect of eccentricity and gyro drift are simulated.