Convex Optimization-Based Model Predictive Control for Mars Ascent Vehicle Guidance System

Dear Editor, This letter proposes a convex optimization-based model predictive control (MPC) autonomous guidance method for the Mars ascent vehicle (MAV). We use the modified chebyshev-picard iteration (MCPI) to solve optimization sub-problems within the MPC framework, eliminating the dynamic constraints in solving the optimal control problem and enhancing the convergence performance of the algorithm. Moreover, this method can repeatedly perform trajectory optimization calculations at a high frequency, achieving timely correction of the optimal control command. Numerical simulations demonstrate that the method can satisfy the requirements of rapid computation and reliability for the MAV system when considering uncertainties and perturbations.

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Publication Details

Journal
IEEE/CAA Journal of Automatica Sinica
Published
2024-12-24
DOI
https://doi.org/10.1109/jas.2024.124587
Citations
3
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
3.90
Controls
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article

Convex Optimization-Based Model Predictive Control for Mars Ascent Vehicle Guidance System

Yanning Guo, Guangfu Ma, Yueyong Lyu, Kun Li et al.
3 citations
IEEE/CAA Journal of Automatica Sinica
Spacecraft Dynamics and Control
3.90
article

Convex Optimization-Based Model Predictive Control for Mars Ascent Vehicle Guidance System

Yanning Guo, Guangfu Ma, Yueyong Lyu, Kun Li, Guangtao Ran
article en
3 citations

Abstract

Dear Editor, This letter proposes a convex optimization-based model predictive control (MPC) autonomous guidance method for the Mars ascent vehicle (MAV). We use the modified chebyshev-picard iteration (MCPI) to solve optimization sub-problems within the MPC framework, eliminating the dynamic constraints in solving the optimal control problem and enhancing the convergence performance of the algorithm. Moreover, this method can repeatedly perform trajectory optimization calculations at a high frequency, achieving timely correction of the optimal control command. Numerical simulations demonstrate that the method can satisfy the requirements of rapid computation and reliability for the MAV system when considering uncertainties and perturbations.

IEEE/CAA Journal of Automatica SinicaVol. 12(10)
Harbin Institute of Technology (CN)
Climate action
Openalex Percentile: Top 6%
Spacecraft Dynamics and Control
3.90
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Convex Optimization-Based Model Predictive Control for Mars Ascent Vehicle Guidance System — Yanning Guo, Guangfu Ma, et al. · IEEE/CAA Journal of Automatica Sinica (2024) | TGRS Research Map | TGRS