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attitudecontrolofaircraft
- 本文首先建立了航天器姿态动力学及运动学方程，该方程具有较强的非线性特性。通过将状态耦合部分作系统干扰项的处理，使原来的非线性模型转化为线性模型加非线性干扰的形式，从而得到了更加简单明了的姿态控制系统的表达式。 在应用滑模变结构原理对系统进行控制器设计时，首先通过二次型最优法求出了最优滑动面，在此基础上，利用自适应滑模控制原理，设计出了合适的系统控制律。 最后，运用所设计的姿态控制系统对某航天器进行数值仿真，并对仿真结果进行了分析。仿真结果很好地体现出所设计的变结构控制器的优点，并成功地
srg-jioadu-youhua
- 开关磁阻电机的最优开关角控制规律的研究 开关磁阻电机的最优开关角控制规律的研究-SRM Optimal switching angle control law of the SRM optimal switching angle of the control law Research
algeorithm-program-for-invented-pendulum
- 续上一个程序的线性控制律的滑模变结构控制源代码，在二级摆上进行实验，调试运行正确。-continued on a linear process control law SMVSC control of the source code, in the top two experiments Debugging operating correctly.
m
- 中文的基于matlab得直升机模拟，做的还行，就是有点假，实现没有只有他自己知道。-A helicopter flight control system simulation software package was introduced, which was developed on MATLAB 6.5. Several unit math models and system simulation were introduced. The software has made good e
backstepping_control
- 针对三维运动机器手臂的控制，设计基于反步控制法的控制器。-For three-dimensional motion of a robot arm control, step control law design is based on the anti-controller.
ALINEASimulation
- application of ALINEA local feedback control law to control freeway for simulation
Aircrgorithm
- 飞行器全包线控制律算法实现及仿真Aircraft full envelope control law and simulation algorithm-Aircraft full envelope control law and simulation algorithm
Position-Sensorless-Control-for-PM
- ：针对电动汽车永磁同步电机无位置传感器控制系统，在两相静止坐标系( —B)内将滑模观测器法 与MRAS结合，提出了基于模型参考自适应的滑模观测器，并利用自适应律估计永磁同步电机的转子速度。仿真 和试验表明无位置传感器控制方法是切实可行的。 关键词：电动汽车永磁同步电机无位置传感器控制 自适应滑模观测器-This paper presents a new adaptive slid—mode observer for electric vehicle permanent magnet
Research-of-PMSM--Control
- 文以永磁同步电机为对象，采用矢量控制方案，首先我们研究了基于PI 的控制算法，在仿真基础上指出了PI 算法存在的一些不足。 在此基础上我们研究了基于扩张状态观测器（ESO）前馈补偿和线性比例反馈控制的永磁同步电机速度环控制算法， -Taking PMSM as the controlled plant, this paper studies the control system based on vector control, first, the servo control s
flightcontrol
- 本代码是用matlab编写，实现功能为飞控系统控制律的设计。-This code is with matlab, function for the flight control system of control law design
Sliding-Mode-Control-Inverter
- ：对全桥型逆变器的滑模控制方案进行了分析，包括建 立系统的变结构模型、选择滑模切换线和确定控制作用，给 出可到达条件及滑模存在区域等。着重讨论了在实际电路设 计中选择开关面系数和开关频率的原则，并且给出相应的设 计程序。-A sliding mode control scheme for the full bridge buck inverter was analyzed, including modeling the variable structure system,
flying-control-law
- 概述了飞行控制律设计的几种主要方法。通过对比自适应飞行控制律和程序调参飞行控制律,总结 了处于飞行控制器设计领域主导地位的程序调参飞行控制律的主要优点和不足,并就程序调参技术在现代飞控领 域的研究现状及其在某先进飞机中的实际应用进行了介绍。最后,针对现代飞机的飞行特点,展望了程序调参飞 行控制律今后可能的发展方向。 -Summarizes the flight control law design of several major method. By comparing the
Flight-control-Law
- 介绍了飞机纵向和横航向控制律设计，给出了设计过程，设计细节作了详细论述-the control law for logititude and direction is introduced , the design process is gived,the design details is demostrated.
self-tuning-control
- 广义最小方差自校正控制：在求解控制律的性能指标中引入对控制量的加权项，限制控制作用中的剧烈变化。-Generalized minimum variance self-tuning control: control the amount of weighted items, solving the performance of the control law introduced to limit the dramatic changes in the control action.
PID-control-law
- 本例程主要是PID控制率的总调程序，以及P、I、D各控制参数对系统的影响子程序。-This routine is mainly the rate of total tune PID control procedures, as well as P, I, D of the control parameters of the system affect the subroutine.
minimum-variance-control
- 用两种预报方法，即Diophantine方程和Jenibox求广义最小方差控制律，画出闭环输入输出图,matlab程序及结果-Using two forecasting methods, namely Diophantine equations and Jenibox seeking generalized minimum variance control law, the closed-loop input-output diagram draw, matlab procedures and
self-tuning-control
- 两种显示自校正最小方差控制,两种隐式自校正广义最小方差控制律,作业程序和结果-Two display self-tuning minimum variance control, two kinds of implicit self-tuning generalized minimum variance control law, procedures and results
DMC-control
- DMC控制律，显式自校正DMC，隐式自校正DMC仿真例子，MATLAB程序和结果，详细好用-DMC control law, explicit self-tuning DMC, DMC implicit self-tuning simulation example, MATLAB procedures and results, detailed easy
Heli
- 直升机飞行控制律仿真，包含姿态及位置反馈回路，PID控制算法，及模糊控制算法(Helicopter flight control law simulation, including attitude and position feedback loop, PID control algorithm, and fuzzy control algorithm)
control
- the yaw motion of the tanker is described in state space by the equation... find a state feedback control law of the form