摘要
针对某型飞机惯性高度测量存在的问题,引入外部高度信号对其进行阻尼,采取混合高度测量方法,大大提高了该型飞机高度测量的准确性和稳定性。研究结果表明,本方案科学、可行,具有较强的实用性。
Contraposed the problem of the inertial altitude measure of some type of airplane.Used outside height signal to damp it.Adopted mixing measure technique.It greatly improved the veracity and stability of altitude measure.Simulating result proves that the improving design is scientific and feasible,and have more practicability.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第S1期192-194,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
惯性高度
纯惯性高度
混合测量
仿真
inertial altitude
damp
mixing measure
computer simulation