Sliding-Mode Control for On-Orbit Rendezvous with a Fleeing Passive Target on a Circular Capture Trajectory
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EN
Communication dans un congrès avec actes
Este ítem está publicado en
2022 30th Mediterranean Conference on Control and Automation (MED), 30th IEEE Mediterranean Conference on Control and Automation, Jun 2022, Athens, Greece., 2022-06-28, Athènes. 2022-08-01p. 571-576
Resumen en inglés
This paper deals with the design of finite-time controllers for on-orbit rendezvous and capture missions. The objective is to assess the capacity of sliding–mode controllers to control a chaser spacecraft during a capture ...Leer más >
This paper deals with the design of finite-time controllers for on-orbit rendezvous and capture missions. The objective is to assess the capacity of sliding–mode controllers to control a chaser spacecraft during a capture maneuver of a fleeing passive spacecraft. The control solution is based on a variable structure approach that relies on the sliding mode control theory. More precisely, the general super-twisting algorithm is used to control the chaser’s attitude, whereas the control of the relative position between the two spacecraft is based on the simplex-based sliding mode control theory. The method is tested in a full-scaled benchmark that accurately simulates the capture mission.< Leer menos
Palabras clave
Space vehicles
Automation
Attitude control
Propulsion
Benchmark testing
Harmonic analysis
Orbits
Position control
Space vehicles
Variable structure systems
Centros de investigación