saichikine / StatODFinalLinks
Final project for ASEN 6020 Statistical Orbit Determination. Uses Unscented Kalman Filter to estimate spacecraft state with unknown perturbations.
☆17Updated 7 years ago
Alternatives and similar repositories for StatODFinal
Users that are interested in StatODFinal are comparing it to the libraries listed below
Sorting:
- Spacecraft Dynamics Capstone Project (Coursera): Attitude Dynamics and Control of Nano-Satellite Orbiting Mars☆10Updated 5 years ago
- Multi-rendezvous Spacecraft Trajectory Optimization with Beam P-ACO☆39Updated 7 years ago
- Collision Probability Calculation and Optimal Avoidance Control for Spacecraft.☆17Updated 4 years ago
- Master's Thesis: single-phase hybrid differential dynamic programming applied to low-thrust Sun-Earth L1 halo to L2 halo orbit transfers.☆16Updated 6 years ago
- Machine Learning + Spacecraft Trajectory Optimisation☆33Updated 3 years ago
- Simulates two conceptually designed two-stage launch vehicles in a gravity turn that places the payload in the a targetted, circular orbi…☆11Updated 6 years ago
- Fast Trajectory Optimization via Successive Convexification for Spacecraft Rendezvous with Integer Constraints☆36Updated 5 years ago
- FORMFLYT - High fidelity orbit propagation for formation flying control in MATLAB!☆23Updated 3 years ago
- Multi-Objective Low-Thrust Optimizer for Interplanetary Transfers☆35Updated 4 years ago
- An almost fully automated MATLAB CR3BP library.☆26Updated 2 years ago
- Algorithms regarding spacecraft attitude determination and control.☆15Updated 5 years ago
- All Matlab codes from Orbital Mechanics for Engineering Students book☆47Updated 6 years ago
- A toolbox for the main functions used in spacecraft attitude determination and control.☆11Updated 6 years ago
- Simulink model for Quaternion based Satellite Attitude dynamics and control☆13Updated 4 years ago
- ☆30Updated 4 years ago
- you know what it is☆27Updated 7 years ago
- ☆10Updated 5 years ago
- Materials for Graduate Level Celestial Mechanics Class☆23Updated 10 months ago
- Successive Convexification OPtimal conTrol 2.0☆11Updated 4 years ago
- spacecraft orbit calculate☆59Updated 4 years ago
- The implementation of 《Successive Convexification for 6-DoF Mars Rocket Powered Landing with Free-Final-Time》☆15Updated 5 years ago
- Determine the position, velocity, and orbit (in 3D) of satellite with given the initial vector (r0 &v0), using MATLAB☆12Updated last year
- This project implements multiple-interval pseudospectral methods to solve optimal control problems.☆46Updated 8 years ago
- Robust Optimal Autopilot Design for Hypersonic Reentry Thrust Vector Control of Rockets☆26Updated 3 years ago
- Spacecraft Proximity Operations Testbed☆14Updated last month
- Inspired by Orion and the Artemis I mission, this example simulates a lunar mission trajectory in MATLAB and Simulink.☆27Updated 2 years ago
- A set of Lambert's problem solvers☆68Updated last month
- Determination of optimal spacecraft landing trajectories via convex optimization☆19Updated 6 years ago
- ☆12Updated 7 years ago
- A set of routines for data processing related to ORBit Determination(ORBD) of space objects☆18Updated last year