Predictive Control for Spacecraft Rendezvous
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Beschreibung
This brief addresses the design of model predictive control algorithms for performing space rendezvous manoeuvres. It consolidates developments within guidance and control algorithms, with the aim of improving the efficiency, safety, and autonomy of these manoeuvres.
The brief presents several applications of model predictive control to rendezvous manoeuvres, including Ankersen zero-order-hold particular solution1, which provides a realistic thrust profile. It offers new approaches for rendezvous manoeuvres in elliptical orbits, formulating obstacle avoidance constraints, passive safety constraints, and robustness techniques. It also compares finite-horizon and variable-horizon formulations for model predictive control in the context of performance and computational complexity.
Predictive Control for Spacecraft Rendezvous is accessible to academics and students new to the topics of orbital rendezvous and model predictive control, but also presents compelling subject matter for researchers and professionals in the aerospace industry.Offers an overview of model predictive control applied to spacecraft rendezvous manoeuvres Addresses rendezvous manoeuvres in elliptical orbits and the Rendezous Experiment to be flown aboard the ESA PROBA-3 mission Presents a new method for formulating obstacle-avoidance and passive-safety constraints
Autor*in
Afonso Botelho
Themen in »Predictive Control for Spacecraft Rendezvous«
Rendezvous Manoeuvres Model Predictive Control Orbital Mechanics Spacecraft Motion Control Spacecraft Rendezvous Impulsive Control Spacecraft Rendezvous Safety Collision Avoidance Obstacle Avoidance