基于轨迹线性化方法(TLC)及神经网络技术研究了一种新的直接自适应TLC控制方案。
This paper presents a novel nonlinear adaptive control method based on trajectory linearization control method (TLC) and neural networks.
经分析计算与试飞结果表明，对于爬升较缓慢的飞机，本控制方案可实现沿优化性能轨迹上升，并自动转入有利速度巡航。
It is shown that the climbing control plan is applicable to the aircraft with slower climbing according to optimum performance trajectory and automatically fly with optimum cruising velocity.
它为工业机器人在非线性运动学约束条件下的时间最优轨迹规划及控制问题提供了一种较好的解决方案。
It provides a better solution to the problem of industrial robot's time optimal trajectory planning and control under the nonlinear kinematical constraints.
针对三自由度机械手轨迹跟踪问题的仿真实验表明，采用T-S型模糊神经网络的机械手轨迹跟踪自适应控制方案是可行的和有效的。
Simulation results of a 3-DOF industrial manipulator trajectory tracking system are presented to show the proposed control scheme is practical and effective.
采用数据文件插补和在线插补两种方案，解决了拉弯机位移控制中任意曲线的插补问题，实现了任意曲线轨迹的精确控制。
To solve the interpolation problem of random curve, the schemes of data file interpolation and on-line interpolation are used, which proves to be accurate.
基于线性系统跟踪控制理论，利用线性系统中的模型参考跟踪控制的方法设计了一种对指定轨迹进行跟踪的制动方案。
Based on the tracking control theory of linear system, a braking scheme to track a prescribed trajectory is designed by using the model reference approach of linear system.
研究一种新的空天飞行器基于非线性干扰观测器的轨迹线性化飞行控制方案。
A novel nonlinear disturbance observer-enhanced trajectory linearization control (TLC) structure is applied to an aerospace vehicle (ASV).
本文对用微计算机进行连续运动轨迹控制提出了一种新方案，并在绘图仪上进行了试验，取得了预期效果。
This article advances a new plan which explains the continuous path control by microcomputers. This plan has been tested on the plotter, and has achieved the desired results.
提出了一种包含运动学控制器和速度控制器的分层控制方案来解决机器人轨迹跟踪控制中的复杂计算问题。
A hierarchical control strategy which includes kinematical controller and velocity controller is presented to solve the problem of complex calculation in robot trajectory tracking control.
分析了沿最优轨迹飞行的物理原因和基本迎角控制规律，可为滑翔式再入飞行器的最优轨迹方案设计提供依据。
The physical causation of the optimal trajectory and the corresponding angleofattack profile are presented. It is a good reference for schematic trajectory design for gliding type reentry vehicles.
分析了沿最优轨迹飞行的物理原因和基本迎角控制规律，可为滑翔式再入飞行器的最优轨迹方案设计提供依据。
The physical causation of the optimal trajectory and the corresponding angleofattack profile are presented. It is a good reference for schematic trajectory design for gliding type reentry vehicles.
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