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Published on: February 16, 2019
A Robust Observation, Planning, and Control Pipeline for Autonomous Rendezvous with Tumbling Targets.
Keenan Albee1, Charles Oestreich1,2, Caroline Specht3
1Space Systems Laboratory (SSL) and Astrodynamics, Space Robotics and Controls Lab (ARCLab), Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA, United States.
This study presents a complete pipeline for autonomous spacecraft rendezvous with tumbling space debris and defunct satellites. It enables safe docking by estimating target motion and planning robust control strategies for active debris removal.
Area of Science:
- Robotics and Autonomous Systems
- Spacecraft Engineering
- Orbital Mechanics
Background:
- The increasing amount of space debris and non-functional satellites threatens the sustainable use of space, potentially leading to Kessler syndrome.
- Servicing or deorbiting satellites in high orbits and managing tumbling debris presents significant challenges due to unpredictable motion.
- Current rendezvous missions are advancing, but practical solutions for autonomous docking with uncontrolled tumbling targets are undemonstrated.
Purpose of the Study:
- To propose and demonstrate a complete pipeline for autonomous rendezvous and docking with tumbling space targets.
- To develop and integrate algorithms for target state estimation, motion planning, and robust control under uncertainty.
- To address the critical need for active debris removal and on-orbit servicing capabilities.
Main Methods:
- A novel visual estimation algorithm using a 3D time-of-flight camera for remote estimation of target rotational state and axes.
- A nonlinear programming-based motion planning algorithm utilizing offline simulations and a lookup table for on-orbit execution.
- An uncertainty characterization method and a robust tube model predictive controller for guaranteed trajectory tracking.
Main Results:
- Successful simulation of the complete pipeline, from standoff estimation to mating in the target's rotating frame.
- Demonstration of robust control that accounts for target tumble uncertainty and provides translational tracking guarantees.
- Validation of individual components and the integrated system through comprehensive case studies.
Conclusions:
- The proposed pipeline offers a viable solution for autonomous rendezvous and docking with tumbling space objects.
- The integrated approach addresses key challenges in active debris removal and on-orbit servicing.
- The system is being prepared for demonstration on the International Space Station, following successful Astrobee free-flyer tests.
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