The system used INS data to determine the reference trajectory.
该系统利用INS数据进行参考轨迹确定。
Gait designs were divided into two main categories: reference trajectory and natural dynamics.
把两足机器人步态综合方法分为参考轨迹法和自然动力学法两大技术流派。
The existence of the bounded solution of unstable internal dynamics is the key to tracking reference trajectory stably.
研究表明，不稳定内部动态有界解的存在性是非最小相位系统能够稳定跟踪期望输出轨迹的关键。
Then, through solving the slow time-scale problem by optimal control theory, the optimal reduced-order reference trajectory is obtained.
然后，应用最优控制理论得出慢时间尺度上的解，并将其作为降维后的最优参考轨迹；
According to the task, must design a standard return trajectory which is reference trajectory for guidance when a manned spacecraft returns.
载人航天器返回时，根据任务的要求，需要设计一条标准返回轨道，作为制导时的参考轨道。
The constrained predictive controller with consideration of the physical constraints can provide an optimal reference trajectory for tracking controllers.
而约束预测控制器则在考虑机械臂物理约束的情况下，为跟踪控制器提供最优参考轨迹。
The constrained predictive controller with consideration of the physical constraints can provide an optimal reference trajectory for tracking controllers.
详细论述了轨迹跟踪控制器和约 束预测控制器的设计原理。
The nominal trajectory-based techniques include the methods to compute the reentry flight corridor, the reference trajectory and the track law of the reference trajectory.
标准轨道法。 给出了再入走廊的计算方法，阐述了参考阻力加速度-速度剖面的规划和跟踪问题。
Supposing that the reference trajectory is generated by a stable system, the bounded solution of non hyperbolic internal dynamics is existed by using center manifold theory.
假设期望轨迹由某一稳定外部系统产生，利用中心流形的理论，证明了系统内部动态有界解是存在的。
The reference trajectory of common model control (CMC) scheme is a classic second order curve. The parameters of CMC are of very explicit physic meaning and it is very easy to tune for the controller.
通用模型控制(CMC)算法的参考轨迹是一条标准的二阶曲线，该控制器的参数具有明显的物理意义，控制器参数整定方便。
The method in the paper can be used in trajectory CAD as reference.
提供的方法可供弹道的计算机辅助设计参考。
To further reduce calculation cost, multiple computing cycles were defined. The output reference attitude command was used to realize the attitude tracking control of reference attitude trajectory.
为进一步降低算法耗费，定义了计算周期的多个层次，最终给出实时参考姿态指令，用以实现参考轨迹的姿态跟踪控制。
To the known bounded reference input trajectory, it can be proved the closed-loop is BIBO stable, and the output will track the reference input asymptotically.
同时证明，对于已知有界参考输入，多模型自适应控制可以保证闭环系统输入输出稳定，输出渐进跟踪设定值。
A parametric approach is proposed for the satellite trajectory tracking problem by using the eigenstructure assignment theory and the model reference theory of linear systems.
基于线性系统的特征结构配置和模型参考理论提出一种卫星轨迹跟踪控制的参数化方法，设计系统的反馈镇定控制器和前馈跟踪控制器。
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.
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。
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.
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。
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