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haloinca's Projects

astrodynamics icon astrodynamics

All Matlab codes from Orbital Mechanics for Engineering Students book

attitudepropagator icon attitudepropagator

A satellite attitude propagator built upon J2 orbit propagator (with a VRML visualisation option) in Simulink.

bdot-algo icon bdot-algo

This repository works on the matlab implementation of the detumbling algorithm on a cubesat. Detumbling is basically the algorithm used to decrease the speed of the satellite after it is launched in the space.

bintel icon bintel

Repository for the intel drone from Burdick's Group at Caltech

completeattdetsim icon completeattdetsim

Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink

czsc icon czsc

缠中说禅技术分析工具;缠论;股票;期货

formflyt icon formflyt

:earth_asia: :satellite: :earth_asia: :satellite: FORMFLYT - High fidelity orbit propagation for formation flying control in MATLAB!

j2 icon j2

Determination of position and velocity of satellited. J2 effect accounted. Compared with SGP solution.

masterthesis icon masterthesis

My Master Thesis in the area of Data-Driven Control Engineering

nmpc-dclf-dcbf icon nmpc-dclf-dcbf

A collection of work using nonlinear model predictive control (NMPC) with discrete-time control Lyapunov functions (CLFs) and control barrier functions (CBFs) (https://arxiv.org/abs/2109.12313, https://arxiv.org/abs/2105.10596, https://arxiv.org/abs/2007.11718)

osculating2mean icon osculating2mean

Convert osculating orbital elements to/from mean orbital elements using spherical harmonics Earth gravity potential.

spacecraft-control icon spacecraft-control

This was part of Spacecraft Attitude Dynamics and Control course assignment. The task was to design a complete spacecraft ADCS. First, sun sensor, star sensor, and earth horizon sensor were employed as vector measurements. Then SVD method was used as attitude determination algorithm, and Luenberger state observer was used as filtering method. The actuator was three axis reaction wheels, where DCM-based control law was utilized as control algorithm. In this simulink model, de-tumbling and nadir pointing were performed succesfully.

srcl_ffnav icon srcl_ffnav

This repo contains the code developed as part of the Relative Navigation for Formation Flying project with the Spacecraft Robotics and Control Laboratory at Carleton University.

stkcodeexamples icon stkcodeexamples

Example scripts and applications for automating and developing with STK and STK Engine.

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