Pinned Loading
-
Real-time-convex-guidance-rocket-landing
Real-time-convex-guidance-rocket-landing PublicMSc Thesis at Indra on real-time onboard successive convexification (SCvx) with quadratic programming (QP) for powered landing guidance of reusable space launchers
-
Reusable-airborne-launch-system-design
Reusable-airborne-launch-system-design PublicSystem level conceptual design of a reusable space launcher, with responsibility for subsystem integration and overall coordination
MATLAB
-
Spacecraft-guidance-and-trajectory-optimization
Spacecraft-guidance-and-trajectory-optimization PublicEarth–Moon transfer optimization via nonlinear programming and shooting methods (single and multiple shooting, n-body propagation), and continuous-thrust orbit raising using Pontryagin Maximum Prin…
MATLAB
-
Spacecraft-navigation-and-uncertainty-estimation
Spacecraft-navigation-and-uncertainty-estimation PublicState estimation via Unscented Kalman Filter (UKF) and uncertainty propagation leveraging Linear Covariance (LinCov), Unscented Transform (UT), and Monte Carlo (MC) techniques
MATLAB
-
Spacecraft-attitude-control-system
Spacecraft-attitude-control-system PublicSimulink simulation of a spacecraft dynamics to develop closed-loop attitude control algorithms with constant thrust jets, magnetometer, star and Sun sensor
MATLAB
-
Space-systems-modeling
Space-systems-modeling PublicModel of an active thermal control system (solar panels, radiators, DC motor) and of an attitude control system (accelerometer, amplifier, solenoidal valve, ion thruster)
MATLAB
If the problem persists, check the GitHub status page or contact support.