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sldemo_f14
- This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot
Spacecraft_Control_Toolbox
- The Spacecraft Control Toolbox is composed of MATLAB m-fi les and mat-fi les, organized into a set of modules by subject. It is essentially a library of functions for analyzing spacecraft and missions. There is a substantial set of softwa
dcmfromeulerang
- 飞行器姿态角的欧拉角表示方法与余弦矩阵表示方法的matlab转换程序-Aircraft attitude angle of the Euler angle method with cosine matrix methods matlab conversion process
AeroModelHighAlpha
- 飞机大角度攻击的模型仿真程序，描述了在大角度攻击时的姿态控制参数的计算。-Model for large angle of attack aircraft simulation program, described the attack in the large angle attitude control parameter calculation.
Nav
- 利用陀螺仪和加表的输出进行惯导结算，得到飞机的位置，速度，姿态角-Use of gyro inertial navigation and processing the output of clearing the table to get the aircraft position, velocity, attitude angle
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
jielian
- 捷联惯导航姿系统C语言实现，可以方便的得到飞机的飞行姿态。-Navigation position system SIMU program development, you can easily get the aircraft attitude.
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.
e2qaq2e
- 用欧拉角表示的飞行器姿态运动学方程在大角度时会出现奇异现象,而采用四元数来 表示,则可以避免这个问题。因此,飞行器运动学方程都采用四元数来表示。而飞行器的控 制规律都采用欧拉角来表示,且欧拉角表示姿态角比起四元数更加形象,更易于被人理解, 所以,在飞行器控制系统仿真设计的时候,需要四元数与欧拉角之间的转换。给定1 个欧拉 角,对应1 个四元数,因而欧拉角到四元数之间这种一一对应的关系使得欧拉角到四元数的 转换比较容易。但是,1 个四元数通常有1 个或者2 个欧拉角与之对应,它
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
MWCv2.2
- 四轴飞行器控制程序，内含姿态解算与pid算法，并由本人亲自注释，清晰易懂-Four aircraft control procedures, including attitude solution with pid algorithm, by personally comment, lucid
Fuzzycontrol
- 模糊自整定PID控制系统设计与仿真 飞机俯仰姿态保持模糊PID控制 -Fuzzy self-tuning PID control system design and simulation aircraft pitch attitude to maintain Fuzzy PID Control
ANO-MR-F1
- 四轴飞行器程序，含陀螺仪姿态角显示及其控制，稳定易懂，运用PID算法，卡尔曼滤波-Four axis aircraft program, display containing gyro attitude and attitude control, stable and easy to understand, the use of PID algorithm, Calman filter
ins_jiesuan_matlab
- 本程序为捷联惯导的解算程序(由惯性器件的输出解算出飞行器的位置、速度、姿态信息-The program for the sins of the solver (by the output device calculates the inertial solution aircraft position, velocity, attitude information
AIRCRAFT
- 建立了四旋翼飞行器悬停姿态动力学模型，并进行了仿真分析，在开环控制的前提下分析了结构增稳和橡筋阻尼方法对飞行器平台姿态定性的影响，并提出了一种开环控制下实现稳定悬停的策略。-The establishment of a four-rotor aircraft hovering attitude dynamics model and simulation analysis, under the premise of open-loop control analyzes the impact of
fangyiu
- 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，匹配追踪和正交匹配追踪，仿真效率很高的。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Matching Pursuit and orthogonal matching pursuit, High simulation efficiency.
nuigai_v73
- 直线阵采用切比学夫加权控制主旁瓣比，GSM中GMSK调制信号的产生，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。- Linear array using cut than learning laid upon the right control of the main sidelobe ratio, GSM is GMSK modulation signal generation, It comprises aircraft flight attitude control, s
peihou_v34
- 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，非归零型差分相位调制信号建模与仿真分析 ，保证准确无误，是学习通信的好帮手。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, NRZ type differential phase modulation signal modeling and simulation analy
punqing_v70
- 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，包括脚本文件和函数文件形式，毕设内容，高光谱图像基本处理。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Including scr ipt files and function files in the form, Complete set content, basic
Euler-angel-and-quater-control
- 飞机姿态角控制时，基于四元数和欧拉角的位置坐标转换关系，欧拉角控制法同四元数控制方法间的相互转换。-When the aircraft attitude angle control, based on the quaternion and Euler angle of the coordinates of the conversion relationship between the Euler angle control method and quaternion control method