摘要
文中基于捷联寻的制导技术在某火箭中的应用,根据该火箭制导系统的特点,提出了该制导火箭制导控制系统的一种具体设计,并首次在常规的捷联制导中引入了平衡攻角补偿和重力补偿,结合数字仿真结果,验证了制导火箭制导控制系统原理的可行性。
The application that technology of strapdown homing guidance is researched in this article. According to the characteristic of control and guidance system of rocket,a material of design based on the rocket control and guidance is proposed. The balaneeable angle of attack and gravity compensation is created firstly in ordinary strapdown homing guidance system. Accordingly, the simulation data analysis result has indicated this method of control and guidance validity.
出处
《弹箭与制导学报》
CSCD
北大核心
2009年第1期71-72,84,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
导引律
攻角
俯仰角
控制系统
guidance law
angle of attack
pitching angle
control system