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Novel Methodology for Control and Stabilization of Spacecraft with Captured Asteroid, Year 2
Completed
TRL 3 (started at 2, targeting 3)
Description
Development of novel spacecraft guidance control architectures and algorithms that work in conjunction with robot manipulator control for application to ARM mission type. Emphasis will be placed on new mission scenario of controlling the spacecraft while collecting a multi-ton boulder from the surface of a large near-Earth asteroid. Computer simulation demonstration and performance analysis of control and stabilization algorithms.
Benefits
Results of this CIF project, such as first-of-a-kind tools for stabilization and control of a spacecraft-boulder combination and synchronized robotic arm control, will have direct application to NASA and DoD (DARPA, Navy, Air Force) missions for rendezvous with tumbling spacecraft for in-orbit servicing and in-orbit construction.
Details
| Technology area | Robotic Systems > Autonomous Rendezvous and Docking > Robot Control for Vehicle Capture and Berthing |
| Program | Center Innovation Fund: JPL CIF (JPL CIF) |
| Lead organization | Jet Propulsion Laboratory, Pasadena, CA |
| Start date | 2015-10-01 |
| End date | 2016-09-30 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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