학술논문

Adaptive high order sliding mode control for relative positioning and trajectory tracking of spacecraft formation flying
Document Type
Conference
Source
2016 24th Mediterranean Conference on Control and Automation (MED) Control and Automation (MED), 2016 24th Mediterranean Conference on. :1095-1101 Jun, 2016
Subject
Aerospace
Power, Energy and Industry Applications
Robotics and Control Systems
Space vehicles
Mathematical model
Satellites
Earth
Nonlinear dynamical systems
Uncertainty
Sliding mode control
High Order Sliding Mode
Adaptive Control
Spacecraft Formation Flying
Language
Abstract
This paper considers the problem of relative position and trajectory tracking control for spacecraft formation flying. The nonlinear dynamics describing the relative positioning of multiple spacecraft are used to develop a Lyapunov-based, nonlinear, adaptive higher order sliding mode control. The strategy, known as adaptive super twisting sliding mode control law, guarantees convergence to any sufficiently smooth desired spacecraft formation flying trajectory, despite the presence of unknown disturbances. Simulation results illustrate the effectiveness of the proposed control.