oygx210

Pinned Repositories

• ADRC-GIT

  ADRC(Active Disturbance Rejection Control)

  Language:MATLAB11

• ANDY

  Symbolic-Numerical Multibody Toolbox for Nonholonomic, Constrained and Hybrid System

  Language:MATLAB1000

• COpNav-Pseudorange-Measurements-Simulator

  Replicating results from "Observability Analysis of Collaborative Opportunistic Navigation With Pseudorange Measurements" paper. Here, an EKF-based estimator is used to simulator various observability scenarios for a vehicle moving in a unknown dynamic and stochastic envrionment.

  Language:MATLAB6000

• CR3BP-Mission-Analysis-and-Design

  A repository containing Matlab scripts on mission and orbit analysis for the three body problem, dealing with the Circular Restricted Three Body Problem approach.

  Language:MATLAB30

• Guidance-Navigation-and-Control

  Simulation and Implementation of some Guidance, Navigation, and Control Laws on UAV, Quadrotor, and Missile

  Language:MATLAB81

• HGESO

  High-gain extended state observer for a quadrotor UAV

  Language:C++41

• Initial-Condition-Estimation-Sensitivity

  This simulator will look at the sensitivity issues with EKF-based estimation. Incorrectly initializing the estimate states will result in an incorrect state observer.

  Language:MATLAB20

• Satellite-Thermal-Control

  Satellites are exposed to the harsh environment in space, that vary its temperature widely as the satellite orbits around a planet. A thermal control system for a satellite at lower altitudes must be designed to regulate the fluctuations in the temperature. In the current work, a thermal analytical model for an isothermal, single-noded satellite revolving in a Low altitude Planet Orbit has been developed from the fundamental principles. The primary aim of this project is to solve the temperature of the satellite as a function of its orbital position using MATLAB code. Parameters like absorptivity and IR emissivity of the satellite effect the thermal condition of the satellite. Thus, the variation in the temperature of the satellite w.r.t various parameters is observed using MATLAB code to study its thermal effects. The temperature of the satellite, solved using the MATLAB code, returns the temperature, which obtain a reasonable approximation for the satellites at lower altitudes.

  Language:MATLAB3000

• SatelliteOrbitPropagatorAndMissionPlan

  This project can use SGP4 and HPOP models to propagate the satellite orbit and make mission schedules for the payload, such as camera, SAR and data transmitter.

  Language:C7001

• SMC-Toolbox

  Sliding Mode Control Toolbox revisited

  Language:MATLAB33

oygx210's Repositories