Capturing Tumbling Objects in Orbit with Adaptive Tube Model Predictive Control

There is a growing need for sophisticated rendezvous and docking guidance algorithms capable of capturing tumbling, noncooperative objects, e.g., space debris, before they collide with other spacecraft. This capability entails sending a chaser (specialized spacecraft) that attaches to the target (tumbling object) to stabilize or deorbit the noncooperative asset. While rendezvous and docking with cooperative objects has been possible for several decades, advanced strategies for tumbling objects that account for uncertainties in the model parameters of either the chaser or target are still under development. We propose the use of adaptive dynamic tube model predictive control (ADTMPC) for trajectory planning of the chaser for rendezvous and docking with the target. Traditionally, the presence of model uncertainty requires the use of robust guidance techniques that are often conservative, leading to suboptimal performance. The main advantage of our approach is the ability to safely update the prediction model online leading to less conservative trajectories and behaviors without violating safety constraints that include time-varying collision constraints and other standard state or control constraints. The approach relies on computing a suitable robust tracking controller offline and combining it with a set membership identification algorithm that identifies the feasible set of parameters online. Under mild assumptions, we guarantee the system will always satisfy the specified constraints even as the model is changing online. Moreover, our approach can incorporate predictions of how the closed-loop trajectory tracking performance will vary with the designed trajectory. This property, in essence, can be used to inform the guidance algorithm on which maneuvers can be executed without exciting the uncertain system dynamics. We demonstrate our approach for a chaser-target scenario where drag, inertial parameters, and orbit parameters are uncertain.

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Publication Details

Published
2025-03-01
DOI
https://doi.org/10.1109/aero63441.2025.11068695
Citations
1
Primary Topic
Robotic Path Planning Algorithms
Type
article
Field-Weighted Citation Impact
1.28
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article

Capturing Tumbling Objects in Orbit with Adaptive Tube Model Predictive Control

Aaron John-Sabu, Brett T. Lopez
1 citations
Robotic Path Planning Algorithms
1.28
article

Capturing Tumbling Objects in Orbit with Adaptive Tube Model Predictive Control

Aaron John-Sabu, Brett T. Lopez
article en
1 citations

Abstract

There is a growing need for sophisticated rendezvous and docking guidance algorithms capable of capturing tumbling, noncooperative objects, e.g., space debris, before they collide with other spacecraft. This capability entails sending a chaser (specialized spacecraft) that attaches to the target (tumbling object) to stabilize or deorbit the noncooperative asset. While rendezvous and docking with cooperative objects has been possible for several decades, advanced strategies for tumbling objects that account for uncertainties in the model parameters of either the chaser or target are still under development. We propose the use of adaptive dynamic tube model predictive control (ADTMPC) for trajectory planning of the chaser for rendezvous and docking with the target. Traditionally, the presence of model uncertainty requires the use of robust guidance techniques that are often conservative, leading to suboptimal performance. The main advantage of our approach is the ability to safely update the prediction model online leading to less conservative trajectories and behaviors without violating safety constraints that include time-varying collision constraints and other standard state or control constraints. The approach relies on computing a suitable robust tracking controller offline and combining it with a set membership identification algorithm that identifies the feasible set of parameters online. Under mild assumptions, we guarantee the system will always satisfy the specified constraints even as the model is changing online. Moreover, our approach can incorporate predictions of how the closed-loop trajectory tracking performance will vary with the designed trajectory. This property, in essence, can be used to inform the guidance algorithm on which maneuvers can be executed without exciting the uncertain system dynamics. We demonstrate our approach for a chaser-target scenario where drag, inertial parameters, and orbit parameters are uncertain.

University of California, Los Angeles (US)
Climate action
Openalex Percentile: Top 18%
Robotic Path Planning Algorithms
1.28
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Capturing Tumbling Objects in Orbit with Adaptive Tube Model Predictive Control — Aaron John-Sabu, Brett T. Lopez · (2025) | TGRS Research Map | TGRS