Session

Poster Session 2

Location

Salt Palace Convention Center, Salt Lake City, UT

Abstract

Summary: Multi-satellite coordinated missions can improve upon larger solitary satellite missions through greater flexibility, efficiency, scalability and redundancy. This study considers a more diverse approach to in-orbit motion coordination that reduce dependence on communication links and absolute position references. The non-linear relative equations of motion applied to a chief satellite and a deputy target in the LEO orbit are considered and a feedback control system to facilitate multi-satellite relative motion coordination is designed. The feedback controller relies on on-board optical sensor measuring optic flow signal, similar to the bio-inspired feedback-controlled systems used for various aerial operations. Performance in orbit is analyzed by means of multiple numerical simulations on a rendezvous scenario with a target in LEO orbit. A ground-based experimental testbed is designed for validation of the feedback control framework for space- borne optical systems.

Document Type

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Aug 12th, 9:00 AM

Orbital Motion Coordination Using Bio-Inspired Optical Sensing and Feedback

Salt Palace Convention Center, Salt Lake City, UT

Summary: Multi-satellite coordinated missions can improve upon larger solitary satellite missions through greater flexibility, efficiency, scalability and redundancy. This study considers a more diverse approach to in-orbit motion coordination that reduce dependence on communication links and absolute position references. The non-linear relative equations of motion applied to a chief satellite and a deputy target in the LEO orbit are considered and a feedback control system to facilitate multi-satellite relative motion coordination is designed. The feedback controller relies on on-board optical sensor measuring optic flow signal, similar to the bio-inspired feedback-controlled systems used for various aerial operations. Performance in orbit is analyzed by means of multiple numerical simulations on a rendezvous scenario with a target in LEO orbit. A ground-based experimental testbed is designed for validation of the feedback control framework for space- borne optical systems.