计算机仿真表明，遗传算法可以方便地得到全局最优解，故控制器可以快速稳定地跟踪预定航向，且系统具有较好的鲁棒性。
Computer simulation proves this algorithms can easily get the optimum solution, so the controller can trace the course quickly and smoothly, and the system has good robustness.
本文详细地介绍了用Z- 80微型计算机对自动驾驶仪航向稳定回路，进行半实物仿真试验研究的全过程。
In this paper a complete investigation process of the partial physical simulation test about the lateral channel of stability of an autopilot with the Z-80 microcomputer is introduced in detail.
研究解决无尾布局横航向稳定性的气动力措施。
To study the way to settle the yawing and rolling stability.
一旦稳定了，航向一个安全的路径并且排除这些纠结。
Once stabilized, steer on a safe course and kick our the twists.
根据导弹与目标之间的相对运动方程，应用李雅普·诺夫稳定性理论设计一种新的导弹航向平面导引律。
According to the dynamic equation of relative motion between the missile and the target, Lyapunov stability theory is used to design a new yaw plane guidance law for missiles.
通过舵面的不同组合，用于纵向、横向和航向稳定与操纵控制。
The longitudinal, lateral and direction of this configuration can be controlled through the combination of different control devices.
进而通过建立预测模型，并结合广义预测控制的算法达到航向保持的目的，且具有较好的稳定性和鲁棒性。
A generalized predictive control algorithm is developed with the predictive model to realize the course maintenance with stability and robustness.
进而通过建立预测模型，并结合广义预测控制的算法达到航向保持的目的，且具有较好的稳定性和鲁棒性。
A generalized predictive control algorithm is developed with the predictive model to realize the course maintenance with stability and robustness.
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