Quaternion-Based Generalized Super-Twisting Algorithm for Spacecraft Attitude Control

The separation between generalized force control and actuator-force allocation makes the control tuning independent, to a certain extent, of the charac- teristics of the force

from an initial attitude and angular velocity to a final attitude and angular velocity in minimum time, using two independent control torques [7], and a second where the objective

An algorithm for model-based reinforcement learning is proposed, which uses safe exploration to inform a model of unknown dynamics, and which utilizes control barrier functions in

This paper investigates attitude control with a time-varying reference for a spacecraft model actuated by reaction wheels and magnetorquers, showing (a) an analytical solution

A uniform semiglobal exponential stability (USGES) proof for a time-varying vector field guidance law used for path-following control of vehicles is presented.. A sliding mode

In this test case, a control hardware in the loop setup was used in ICCS RI in order to test a DSO’s control algorithm of a Non-Interconnected Islanded Power System (NIIPS) in

A real time simulation platform is used to control and monitor the the following: • Dc voltage of the grid emulator • Island mode control of the hardware converter • Simulation of

In order to perform reasoning the behaviour models shall have access to data about the simulated environment and react to events in the simulated environment, where the