简要介绍了无线电指令制导的概念和特点。
The conception and characteristics of wireless command guidance are briefly introduced.
复合控制采用对制导指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和直接力控制子系统。
By means of guidance command decomposed forwardly, the combined control system is divided into two parallel subsystems: the aerodynamics subsystem and the direct force subsystem.
采用解析计算的形式预测弹头落点，利用非线性最小二乘方法搜索最优横向力，从而获得制导指令。
The analytical calculation of form, using penetration forecast method of nonlinear least squares search optimal lateral force, thus guidance commands was gain.
将斜率估计结果代入EKF，得到滤除天线罩误差影响的系统状态量估计结果并形成制导指令。
The estimated results of the slopes are introduced into the EKF to get state estimations without radome interference which generates the guidance law command.
文中详细阐述了该制导律的设计过程，给出了制导指令，并对该制导律的性能进行了仿真分析，验证了该制导律的可行性。
This paper expounds the guidance law is presented, the design process, and the guidance command guidance law of performance, the simulation analysis verified the feasibility of the guidance law.
弹上无线电设备接收并译出各种指令后，经自动驾驶仪控制舵面的转动，从而达到控制导弹飞行的目的。
The wireless equipments receive and decode various instructions, and then the fin is commanded to turn by the autopilot, thus the purpose of control the missiles is achieved.
为了实现反舰导弹的大空域变轨，提出了一种三维虚拟目标比例导引律。该导引律利用简单的控制指令就能控制导弹完成复杂的大空域变轨。
In order to realize large airspace transfer orbital trajectory of an anti-ship missile, a 3-dimensional virtual target's proportional navigation guidance (PNG) law is proposed.
为了实现反舰导弹的大空域变轨，提出了一种三维虚拟目标比例导引律。该导引律利用简单的控制指令就能控制导弹完成复杂的大空域变轨。
In order to realize large airspace transfer orbital trajectory of an anti-ship missile, a 3-dimensional virtual target's proportional navigation guidance (PNG) law is proposed.
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