oygx210 Goto Github PK

279c_dragon

Final project files for Stanford AA279C, Spacecraft Attitude Determination and Control.

3-dof-helicopter_modeling-identification-verification

三自由度直升机具有典型的欠驱动、非线性、模型不确定因素与外部干扰作用明显等特点, 作为机器人运动规划与鲁棒控制技术验证的理想平台, 近年来得到国内外知名研究机构的广泛关注。然而, 由于目前文献中缺乏完整和精确的动力学与执行机构模型, 严重制约了先进运动规划与控制算法和其他算法的全面综合对比研究. 对此, 针对测角精度有限的三自由度直升机教学与科研平台, 从多刚体系统的视角, 开展三刚体动力学建模、多通道耦合动力学参数辨识、电机- 螺旋桨升力组件特性辨识、模型线性化处理与分析、模型特性验证等全链条工作, 最终获得了可以直接服务基于模型控制设计的benchmark模型, 并从模型描述平台特性的完整性、精确性和系统性三个方面,开展了大量对比实验. 基于该benchmark模型, 设计并实验验证了经典的“前馈+LQR反馈”角轨迹跟踪控制器, 获得的角轨迹跟踪控制精度水平可作为其他高精度算法的对标对象.

3dof-acs-sim_nonlinearcontroller

3 DOF Attitude Control Simulation of a spacecraft using a Reaction thruster control system

42

Simulation for spacecraft attitude control system analysis and design

560finalproject

Advanced Spacecraft Controls DGVSCMG

6-dof-simulation---orbit-attitude-tracking

This is a 6-DOF Spacecraft Orbit and Attitude Simulation that utilizes two controller (1 for orbit & 1 for attitude), one simplex optimization method implementation, a PWPF modulator, and ode45 (RK 4-5) numerical integration to simulate a closed-loop control system for the given desired attitude, orbit, and initial conditions of just about any particular Space Mission the user chooses.

6-dof_singularity_avoidance_algorithm_using_dual_quaternion

6014_p2

optimal rendezvous guidance

6dof_manipulator_robot_simulation

6dof_satellite_simulation_using_matlab-simulink

6ucubesat

This repository contains two versions of 6U CubeSat Attitude Control System in SpeAR, AADL/AGREE, and Simulink/Simulink Design Verifier: a basic model and an RTA model. The basic model utilizes a PID controller for the controller block, while the RTA model controller utilizes a RTA controller design that includes 3 separate components: unverified controller, verified controller, and decision module.

aa273

aa279b

Reentry Analysis for Mars Sample Return

acados

Fast and embedded solvers for nonlinear optimal control

acsiom-ik1

C++ library for solving serial robot kinematics using dual quaternions

active-noise-cancellation

Active noise cancellation using various algorithms (FxLMS, FuLMS, NLMS) in Matlab, VST and C

active-noise-cancellation-system

LMS, RLS, QR-RLS based FIR adaptive filter for active noise cancellation with and without quantization effects.

activesetctlalloc

C-code and assorted tests for solving bound constrained control allocation problems

actuator-fault-tolerant-multi-controller-scheme

Fault diagnosis based on set separation

adaptive-control

Adaptive control methods developed by Karl Johan Åström and Björn Wittenmark from the 70-80's for industrial use

adaptive-filtering

MATLAB files to implement all Adaptive Filtering Algorithms in this book.

adaptive-gyro-filtering

adaptive notch filtering of gyro data to suppress motor noise

adaptive-mesh-refinement

An adaptive mesh refinement algorithm for MATLAB

adaptive_adrc

The altitude control of a quadrotor unmanned aerial vehicle is treated using its altitude dynamics in hover mode. An LMS-based Adaptive Active disturbance rejection control (AADRC) is proposed to compensate for disturbance effects resulting in smoother control.

adaptive_and_fault_tolerant_flight_control_systems

Adaptive and fault tolerant flight control with Adaptive Neural Networks

adaptivecruisecontrol

A PID (Proportional Integral Derivative) controller for vehicle adaptive cruise control

adaptivecruisecontrol-1

(C/C++) Управление скоростью грузового автомобиля с учетом продольного профиля дороги с целью оптимизации расхода топлива.

adcs

Attitude Determination and Control System Simulation

adcs-software

Attitude Determination and Control Subsystem (ADCS) of EUS-1

adcs_jm

Attitude determination and control system of a CubeSat