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LaserCommunicationSimulationSystem
- 建立GEO和LEO的轨道，并计算他们间方位角和俯仰角速度及加速度，多普勒频移等重要参数。-established GEO and LEO orbits, and calculate their azimuth and pitch between angular velocity and acceleration, Doppler frequency shift and other important parameters.
jtwd
- 电力系统静态稳定计算一般采用小干扰法，即首先计算近似的线性微分方程组系数矩阵的特征根。然后根据特征根在复平面上的特性，判别电力系统运行的稳定性 操作说明： 请输入初始功率S0，形如a+bi 请输入无限大系统母线电压V0 请输入系统直轴等值电抗的大小Xd 请输入同步电角速度 请输入惯性时间常数Tj 请输入综合阻尼系数D-static power system stability calculation generally use small interfering, f
EWTS82
- ewts avr驱动程序 角速度传感器 104为秒-ewts avr driver angular velocity sensor to 104 seconds
Strapdown
- 一、数据说明： 1：惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。 初速度为v0=[0.000048637 0.000206947 0.007106781]，飞行高度不变。 2：jlfw中为600秒的数据，陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。 3：初始姿态角为[0.120992605 0.010445947 91.637207]（俯仰，横滚，航向,单位为度）, jlfw中保存的为比力信
51-lcd-mpu6050(1)
- MPU6050的测试程序，融合加速度与角速度的传感器-MPU6050 the test procedures, integration of acceleration and angular velocity sensor
Timers2-6.6
- 基于陀螺仪原理的惯性导航程序 用于测量量角速度-Based on the principle of gyroscope inertial navigation procedures used to measure the amount of angular velocity
jjooohhhnnneeyy
- 用c++编程求解分析四杆机构的运动分量。包括各杆的线速度，加速度，角速度，转过的角度等。-With c++ Programming analysis of four institutions to solve the sports component. Including the pole line speed, acceleration, angular velocity, the angle of turn and so on.
integration_of_attitudes
- 利用三轴角速率型号和三轴加速度计信号结合扩展卡尔曼滤波实现三个姿态角度的融合-The use of three-axis angular velocity model and three-axis accelerometer signal extended Kalman filter combined with the realization of the integration of the three attitude angles
angularvelocitymatching
- 本人的呕心力作：角速度匹配传递对准matlab程序！绝对没有问题，先运行1，再运行2！-Nausea my works: angular velocity matching transfer alignment procedures matlab! Absolutely no problem to run 1, run 2!
pidsr
- PID用于机器人路径控制的MATLAB程序,路径选择是一个简单的正弦函数.控制参数是速度和角速度.-PID control for robot path MATLAB program, the path of choice is a simple sine function. Control parameter is the speed and angular velocity.
HW
- 介绍陀螺的应用。工作原理等。定量的分析陀螺进动的角速度。-Introduced the gyroscope applications. Such as the working principle. Quantitative analysis of the angular velocity gyroscope precession.
linear
- 倒立摆模型的局部线性化 设倒立摆的摆角范围为[-15,15]度，摆角角速度范围为[-200,200]度/秒，摆角角加速度范围为[-200,200]度/秒2，采用三角形隶属函数对摆角和摆角角速度进行模糊化，摆角初始状态为[0.2,0]。-Inverted pendulum model of the local linear-based inverted pendulum swinging angle of the range of [-15,15] degrees angle angular
RRPAnalysis
- 对机械原理中连杆机构RRP及RPR结构进行分析，包括（角）速度、（角）加速度及（角）位移计算-On the mechanical principle of RRP and RPR linkage analysis of the structure, including the (angular) velocity, (angle) and acceleration (angular) displacement calculation
invertedpendulum
- 倒立摆是一种复杂、时变、非线性、强耦合、自然不稳定的高阶系统，许多抽象的控制理论概念都可以通过倒立摆实验直观的表现出来。基于人工神经网络BP算法的倒立摆小车实验仿真训练模型，其倒立摆BP网络为4输入3层结构。输入层分别为小车的位移和速度、摆杆偏离铅垂线的角度和角速度。隐含层单元数16个。输出层设置为1个输出单元。输入层采用Tansig函数，隐含层采用Logsig函数，输出层采用Purelin函数。用Matlab 6.5数值计算软件对模型进行学习训练，并与线性反馈控制逻辑算法对比，表明倒立摆控制B
081208
- 基于MATLAB软件的交流永磁同步电机调速系统研究 介绍了一种采用磁场定向理论控制交流永磁同步电机的调速系统，应用现代控制理论对 电机直交轴耦合分量进行了解耦，并利用经典控制理论设计了电流环和角速度环调节器。MATLAB 仿真 结果证明了该方法的有效性，但系统调试时仍需根据具体情况适当调整以得到更理想的效果。-MATLAB software based on the exchange of permanent magnet synchronous motor speed contro
satelite
- 通过卫星的测量方程和状态方程来求解卫星的姿态。包括四元数，角度，角速度等等。-By satellite measurements to solve equations and state equations of satellite attitude. Including the quaternion, angle, angular velocity and so on.
variableangularvelocitymodelwithEKF
- 在飞机无源跟踪中，用扩展卡尔曼滤波算法来实现平面变角速度模型。-Passive tracking the aircraft, using extended Kalman filter algorithm to achieve the flat model of variable angular velocity.
xxx
- 用matlab来制作卫星绕地球做周期运动的动画，改变卫星的角速度的初值，可以画出圆形，椭圆形，逃逸轨迹。-Using matlab to produce satellites orbiting the earth to do periodic motion animation, change the initial angular velocity of the satellite, you can draw round, oval, escape trajectory.
ForcedPendulum
- This simulink model simulates the damped driven pendulum, showing it s chaotic motion. theta = angle of pendulum omega = (d/dt)theta = angular velocity Gamma(t) = gcos(phi) = Force omega_d = (d/dt) phi Gamma(t) = (d/dt)omega + omega/Q
sc_attitude-master
- Goal of this project is to simulate the rotational motion of a spacecraft in orbit. Plots of Euler angles and polhode curves (angular velocity time histories) are generated. Equations of Motion included in this package are for a rigid body in a torqu