搜索资源列表
V0.76g
- 四旋翼飞行器飞行控制系统源代码，德国MK四轴V0.76版-MK code
Flight_Attitude_Control_Simulation
- 用LabVIEW实现的“飞行姿态控制仿真”。内有vi：俯仰和滚转控制器、航向控制器、键按下增大、键盘操作、姿态角误差转换、阻尼器。还有9个显示vi和12个模型vi。 飞行控制的目的主要是通过控制飞行器的姿态和轨迹来完成飞行任务，然而飞行轨迹很大程度由飞行姿态决定。可见飞行器姿态控制，在整个飞行控制系统中处于重中之重的地位。飞行姿态控制的好坏直接关系到飞机能否安全、平稳、快速的地飞行。与其它控制系统一样，可用稳定性和动稳态性能来衡量控制效果。稳态时，要使飞行器姿态足够接近所需的飞行姿态，才
KK-V5.5-Final
- KK四轴飞行器-KK飞行控制程序源文件-KK CONTROL DIY BOARD SOURCE DATA
dgao
- 飞行器纵向回路姿态控制系统中阶跃干扰时定高平飞-Aircraft vertical loop attitude control system in step interference Gaoping set to fly
feixingqi
- 对飞行器飞行情况的c++简单实现过程，主要利用visual C-Pairs of aircraft flown by the c++ simple implementation process
Wind_Turbine_model
- 风向扰动模型，用与模拟飞行器数值仿真分析中风的数学模型描述-Wind disturbance model, using numerical simulation analysis and simulation of stroke aircraft mathematical model descr iption
四旋翼飞行器
- 四轴飞行器基本原理，文件讲述了四轴飞行器的一些基本知识。(Fundamentals of four axis aircraft)
stm32四轴
- 四旋翼飞行器程序，原理图，电路图还有遥控器的原理图(Four rotor remote control program)
with_camera_trajectory
- 飞行器simulink6dof仿真软件，供大家参考使用(matlab simulink code for aircraft 6dof kinematic calculating)
四旋翼飞行器模型文件
- 四旋翼飞行器3D打印模型stl文件，包括起落架和电池盒，可以直接打印(Four rotor aircraft 3D printing model STL file)
匿名开拓者Pro飞控源码、原理图
- 飞行器开源及其示范典例，轻轻松松，从入门到精通，不再为开源而烦恼(Open source vehicle)
Crazepony开源四轴飞行器
- 开源四轴飞行器，单次飞行9分钟，基于stm32(Open source four axis aircraft, single flight 9 minutes, based on stm32)
四旋翼飞行器动力学建模与简单PID控制
- 四旋翼飞行器的建模与PID调控，利用simulink进行系统的仿真，主要是动力学仿真，计算结果较为准确(Modeling and PID control of four rotor aerocraft)
再入飞行器射程优化
- 高速再入飞行器射程最大优化，采用单纯形法。(The maximum range optimization of the high speed reentry vehicle is made by the simplex method.)
北航《多旋翼飞行器设计与控制》
- 北京航空航天大学的多旋翼飞行器的PPT压缩包，对于想学飞控的玩家很有用(The PPT of the Beihang University's multi rotor aircraft is very useful for players who want to learn flight control.)
MiniFly V1.1
- MiniFly四轴飞行器固件1.1源码：包括STM32F411源码和STM32F103源码(MiniFly Four axis aircraft firmware 1.1 source code Include STM32F411 source code and STM32F103 source code)
STM32F103四轴飞行器源码
- 基于STM32F103的四轴飞行器源码，包含遥控端与飞行端(Source code for four axis aircraft based on STM32F103)
Clear
- 通用高超声速飞行器纵向模型为研究对象，并针对线性化模型，分别采用极点配置、LQR以及 三种方法设计控制器以改善系统的性能。(The general hypersonic vehicle longitudinal model is the research object. Aiming at the linearized model, pole placement, LQR and three methods are used to design the controller to improve
源程序
- 用matlab编写的代码，用于实现飞行器的一致性状态(The code is used to achieve the consistency of the aircraft)(The code written in MATLAB is used to achieve the consistency of the aircraft.)
附录
- 2020年F题--飞行器质心平衡供油策略优化的相关编程程序，该程序针对磁体有良好的供油效果(F question 2020 -- Programming program for optimization of oil supply strategy for aircraft centroid balance. This program has a good oil supply effect for magnets)