搜索资源列表
nizhuan
- 发射系下飞行器九参数计算，包括位置，速度，姿态-aircraft fired nine-under parameters, including location, speed, attitude
flysimulation
- 基于空间飞行器的姿态仿真源程序，仿真表明非常的准确。
trace3
- 飞行器航迹曲线,三维空间仿真,包括直行,爬升,转弯,俯冲等等运动姿态
The-flying-3D-deplay
- 飞机三维飞行姿态显示例程。内涵有客机、战斗机、直升机三种飞行器模型。-Three-dimensional aircraft flight attitude display routines. Connotation of aircraft, fighter aircraft, helicopters, three kinds of aircraft models.
connect--STK
- 本文介绍如何用stk/connect模块，实现接收当前飞行器质心、姿态数据及动作指令，驱动stk/VO模块实现近实时演示。-This article describes how to use stk/connect module, receiving the current aircraft mass, attitude data and motion commands to drive stk/VO module to achieve near real-time demonstration.
imu-opengl
- 这是在windows上运行的关于IMUopengl应用程序，适合飞行器的姿态实时表达-this is a program about imu s performance by opengl
EKF_MEMS
- 姿态信息是飞行控制中最关键的参数之一,因此姿态测量成为飞行控制系统首要解决的问题。利用多MEMS传感器研制了一种微型姿态测量系统。利用三轴MEMS加速度计和三轴MEMS陀螺数据,由方向余弦矩阵的姿态表示形式推导了扩展Kalman滤波方程,解算出飞行器的俯仰角和横滚角 设计专家系统判断飞行器的运动状态,并根据该状态调整滤波算法中的测量噪声矩阵,使系统可同时满足静态情况和动态情况的使用 利用空速和高度数据对俯仰角进行修正,利用GPS解算航向角。将实验结果与国外最新 的商用自动驾驶仪的姿态结果进行
Euler-equation
- 提出了一种解决欧拉方程奇异性的工程算法，从飞行器运动方程人手，推导出具体计算公式．并进行了数值计算验证。该方法无论是理论分析还是工程计算都证明是可行，没有发现原理缺陷和方法误差，不会产生奇异性，在飞行器仿真、模拟和姿态控制中具有普遍的应用和参考价值。-This paper introduces a new method to solve the singuIarity of Euler equation．
44
- 用于飞行器自动控制的算法计算， 融合三轴加速度计和三轴陀螺的数据融合计算，得出飞行姿态-For aircraft automatic control algorithm, integrated three-axis accelerometer and three-axis gyro data fusion calculations, flight attitude
daima
- 课设作业，包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角-Attitude control of spacecraft Contains the pitch angle, roll angle，Tilt angle, sideslip angle
ars
- 用于四轴飞行器的姿态算法，内含各种矩阵加减乘转置、求逆等运算，及姿态kalman滤波算法，可适用于低速旋翼机的姿态导航-For four-axis spacecraft attitude algorithm, containing a variety of matrix addition and subtraction to multiply the transpose and inverse operations, and attitude Kalman filtering algorithm
zitai
- 空间飞行器三轴稳定姿态动力学仿真，三轴稳定姿态动力学仿真-Stable attitude dynamics simulation of the space vehicle three weeks
四旋翼matlab仿真
- 简单的PID控制四旋翼飞行器，姿态采用PID控制，内有四旋翼模型，电机模型
ADC_4PWM_3_Done
- DSP TMS320F2812的四轴飞行器控制程序，包含四路PWM输出，AD采集，及陀螺仪和加速度计的数据融合代码，姿态调整采样简单的PID控制算法-DSP TMS320F2812 four shaft vehicle control program, including four road PWM output, AD collection, and gyroscope and accelerometer data fusion code, attitude adjustment sampli
flight
- 完成飞行器的纵向姿态仿真。有simulink模型。-Longitudinal attitude of complete aircraft simulation. Simulink model.
degital
- 本程序实现轨迹生成。基于的原理是飞行器位置和姿态解耦，对其进行独立设计，通过反解出惯性器件信息，从而用于导航。-The program trajectory generation. Based on the principle of the aircraft position and attitude decoupling its independent design, the inverse solution inertial devices used for navigation.
mu_autoland_synthesis
- 高超飞行器纵向三自由度模型，可用于线性化研究，进行姿态控制设计-Hypersonic vehicle longitudinal three-degree-of-freedom model can be used for linearization study, attitude control design
4x_mb_scr_code
- 微四轴飞行器飞控源码，姿态检测以及PID姿态控制，以及mpu6050的以及地磁传感器的驱动程序。-Micro Four aircraft flight control source, gesture detection, and PID attitude control, and mpu6050 as well as geomagnetic sensor drivers.
INS-solver
- 由惯性器件的输出解算出飞行器的位置、速度、姿态信息-The output from the inertial device solves for the aircraft position, speed, attitude information