Online Trajectory Generation for Space Manipulator via Nonlinear Model Predictive Control

In this paper, a novel online trajectory planning strategy for a satellite equipped with a robotic arm is presented. This problem is tackled using a nonlinear model predictive control approach, and the result is a flexible trajectory generation strategy that is able to adapt in real time to unseen scenarios and time-varying mission objectives. First, the kinematic and dynamic equations of the system are derived with particular attention with respect to representation singularities and computational efficiency. Then, the trajectory generation problem is written in the form of a constrained optimization problem taking into account actuators saturation and potential collisions with itself and the target object to be grasped. In the last part, multiple simulation scenarios are analyzed to verify the performance and effectiveness of the proposed solution.

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Publication Details

Journal
Journal of Guidance Control and Dynamics
Published
2025-11-25
DOI
https://doi.org/10.2514/1.g009059
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Online Trajectory Generation for Space Manipulator via Nonlinear Model Predictive Control

Angelo Cenedese, Luca Caiaffa, Jacopo Giordano, Mattia Bruschetta
Journal of Guidance Control and Dynamics
Space Satellite Systems and Control
article

Online Trajectory Generation for Space Manipulator via Nonlinear Model Predictive Control

Angelo Cenedese, Luca Caiaffa, Jacopo Giordano, Mattia Bruschetta
article en

Abstract

In this paper, a novel online trajectory planning strategy for a satellite equipped with a robotic arm is presented. This problem is tackled using a nonlinear model predictive control approach, and the result is a flexible trajectory generation strategy that is able to adapt in real time to unseen scenarios and time-varying mission objectives. First, the kinematic and dynamic equations of the system are derived with particular attention with respect to representation singularities and computational efficiency. Then, the trajectory generation problem is written in the form of a constrained optimization problem taking into account actuators saturation and potential collisions with itself and the target object to be grasped. In the last part, multiple simulation scenarios are analyzed to verify the performance and effectiveness of the proposed solution.

Journal of Guidance Control and DynamicsVol. 49(2)
University of Padua (IT)
Openalex Percentile: Top 53%
Space Satellite Systems and Control
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