terminal constraint

Design of H_ ∞ Guidance Law with Terminal Angle Constraint

具有终端角度约束的H∞制导律设计

A model predictive control direct algorithm, which is based on state space for nonlinear system with the unknown parameters and terminal constraint, is presented in this paper. The method avoids computing inverse matrixes, and the computation is reduced.

针对参数未知、具有终端约束的非线性系统，提出了一种新的模型预测控制直接算法，该方法避免了求解逆矩阵，减小了计算量。

A group of ellipsoidal invariant sets is designed off-line, and then constitutes a terminal constraint convex set whose coefficients are taken as on-line optimization variables.

通过离线设计一组椭圆不变集，并将其组合成一个终端约束凸集，其中凸集参数作为在线优化变量。

The union of the control invariant sets is treated as the terminal constraint set of predictive control. The feasibility and stability of the novel dual-mode model predictive control are investigated with both variable and fixed horizon.

本文将控制不变集的并集作为双模预测控制的终端约束集，研究了变时域和固定时域模式下双模预测控制的可行性与稳定性。

The variable structure proportional navigation with terminal angular constraint is utilized, and estimation about the distance rate and distance between missile and target is made, which broke the constraint that passive homing missile can't measure out the distance and distance rate.

采用带落角约束的变结构导引律，对弹目距离及距离变化率进行估计，克服被动寻的导弹不能测距的约束，同时使切换开关增益随时间自适应变化以减小俯冲过载。

The passive homing missile's variable structure proportional navigation with terminal impact angular constraint

带末端落角约束的变结构导引律

First, a terminal constraint is appended at the back of traditional performance index, and corresponding stability theorem is deduced by Lyapunov method.

首先在常规的预测控制性能指标后附加一个人为的终端约束，并利用Lyapunov方法推导了在该情况下确保闭环系统大范围渐进稳定的稳定性定理。

Aiming at a class of nonlinear system with multiple equilibrium points. we present a dual-mode model predictive control algorithm with extended terminal constraint set combined with control invariant set and gain schedule.

本文针对一类具有多个平衡点的非线性系统，结合控制不变集与和增益调度算法，提出了一种基于扩张终端约束集的双模预测控制设计方法。

Following the idea of the performance studies of receding horizon control in control field, a kind of rolling scheduling strategy, in which the sub-problems with terminal constraint are given, is presented for a kind of large scale static single-machine scheduling problem with separable regular criteria.

借鉴控制界对滚动时域控制性能研究的思路，对一类具有可分的正规性能指标的大规模静态单机调度问题，提出了一种子问题带终端约束的滚动调度策略。

This method solves the problems of choosing coefficient matrices, and it does not need to satisfy a terminal state equality constraint.

该方法解决了系数矩阵的选择问题，不需要满足最终状态等式约束。

The feedback form bears a relation to solutions of a Riccati differential equation which corresponds to a problem without terminal constraint and a linear equation of a function matrix.

所得到的反馈形式与相应的无约束问题的Riccati微分方程和一个函数矩阵的线性方程的解有关。

The terminal cost term and terminal constraint region play an important role in the model predictive control ( MPC). MPC with terminal sliding mode constraints for time-delay systems with constraint input is proposed in the paper.

终端约束区域和终端代价项在模型预测控制中起着关键的作用，针对输入受限的时滞系统，提出了终端滑模约束的模型预测控制。

Linear Quadratic Control Problems with a Terminal Inequality Constraint

具有终端不等式约束的线性二次控制问题

Research on Super-Sonic Missile Guidance Plan Based on the Terminal Angular Constraint

基于落角约束的超声速导弹制导方案研究

Robust invariant set is introduced to obtain the terminal constraint set and feasible invariant set for the estimated state.

通过引入鲁棒不变集，构造了关于估计状态的终端约束集和可行不变集，从而实现了输出反馈双模控制，证明了闭环系统的稳定性。

The synthesis method of constrained MPC based on terminal constraint set and terminal cost function guaranteeing stability is studied, and it is shown that the method is in essence an infinite horizon MPC algorithm.

研究了采用终端约束集和终端代价函数的约束MPC的稳定性设计方法，表明了它实质上是无穷时域MPC的一种实现。

An Optimal Guidance Law of Maneuvering Reentry Vehicles with Terminal Angular Constraint

具有终端角度约束的机动再入飞行器的最优制导律

Design of guidance law and controller of missile with terminal angular constraint based on optimal control

基于最优控制的落角约束攻击设计

The robust control for a receding horizon predictive control system with terminal inequality constraint is discussed.

研究了终端不等式约束预测控制系统的鲁棒控制问题。

Optimal Sliding Mode Guidance Law Design with Terminal Angle Constraint for Airborne Dispenser

带末端角约束的机载布撒器最优滑模制导律设计

The machines' load regulation problem with terminal constraint

具有终端约束的机器负荷分配问题

For a class of discrete systems, the problem of MPC with terminal constraint convex set is investigated.

针对一类离散系统，研究了带有终端约束凸集的MPC控制问题。

The Optimal Control Model on Dynamic Input-Output with a Terminal Output Constraint

具有终端产出约束的动态投入产出最优控制模型

The swing up control problem of a single inverted pendulum on an circular rail is discussed. A new optimization is presented by making discrete control law as the design variables and taking terminal constraint condition as the objective function respectively.

研究圆轨单级倒立摆摆起控制问题，以离散控制律为设计变量，以终点约束条件为目标函数，提出了倒立摆摆起控制律的优化算法。

By applying the Lyapunov method and the Taylor formula to the optimal value cost function, the robustness properties of the receding horizon predictive control system with terminal equality constraint is studied.

利用Lyapunov方法及性能指标值关于状态量的泰勒展开，研究了终端等式约束预测控制系统的鲁棒稳定性。

New MPC Controller Based on a Terminal Convex Set Constraint

基于终端凸集约束的新MPC控制器

Variable structure guidance law of reentry maneuvering warhead with terminal angular constraint

带落角约束的再入机动弹头的变结构导引律

The guidance method satisfies terminal angular constraint as reentry vehicle hitting target, but also ensures minimum loss of maneuvering velocity for reentry vehicle.

该方法利用最优控制理论的思想方法，不仅使飞行器命中目标时满足了终端角度约束的条件，而且保证了再入飞行器机动速度损失最小。