Robust Bang-Off-Bang Low-Thrust Guidance Using Model Predictive Static Programming. (November 2020)

• Record Type: Journal Article
• Authors: Wang, Yang; Topputo, Francesco
• Is Part Of: Acta astronautica. Volume 176(2020)
• Page Start: 357
• Page End: 370
• Publication Date: 2020-11
• Subjects: Low-thrust transfers -- Model predictive static programming -- Bang-off-bang control; Astronautics -- Periodicals; Outer space -- Exploration -- Periodicals; Astronautics; Periodicals; 629.405
• DOI: 10.1016/j.actaastro.2020.06.037
• Languages: English
• ISSNs: 0094-5765

Abstract

Abstract: Model Predictive Static Programming (MPSP) has been always used under the assumption of continuous or impulsive control, but never in low-thrust transfers featuring bang-off-bang control. Following the observation that the sensitivity matrix (SM) is discontinuous across the switching time, this work introduces a two-loop MPSP guidance scheme using fuel-optimal trajectories as nominal solutions. In our method, the equations of motion are augmented by the mass costate equation, while the velocity costate is the MPSP control, expressed by a weighted sum of Fourier basis functions. The SM is computed at the switching time by using calculus of variations. Both the MPSP control and the initial mass costate are updated in an inner loop using Newton's method, and continuation is employed in an outer loop to face large perturbations. A sample interplanetary CubeSat mission to an asteroid is used as study case to illustrate the effectiveness and robustness of the method developed. Highlights: A new model predictive static programming method is developed to handle bang-off-bang control. The sensitivity matrix is shown discontinuous across the switching time for low-thrust transfers with bang-off-bang control. Effectiveness and robustness are demonstrated through numerical examples.