Autonomous rendezvous and docking: A commercial approach to on-orbit technology validation

Details Autonomous rendezvous and docking: A commercial approach to on-orbit technology validation Autonomous rendezvous and docking: A commercial approach to on-orbit technology validation

Nov 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991arcr.nasa...31t&link_type=abstract

In its NASA Automated Rendezvous and Capture Review. Executive Summary p 31-32 (SEE N93-21407 07-12)

Computer Science

Autonomous Navigation, Autonomy, Global Positioning System, Navigation Instruments, Orbital Rendezvous, Receivers, Spacecraft Docking, Connectors, Service Modules, Space Commercialization, Transporter

Scientific paper

SpARC, in conjunction with its corporate affiliates, is planning an on-orbit validation of autonomous rendezvous and docking (ARD) technology. The emphasis in this program is to utilize existing technology and commercially available components wherever possible. The primary subsystems to be validated by this demonstration include GPS receivers for navigation, a video-based sensor for proximity operations, a fluid connector mechanism to demonstrate fluid resupply capability, and a compliant, single-point docking mechanism. The focus for this initial experiment will be ELV based and will make use of two residual Commercial Experiment Transporter (COMET) service modules. The first COMET spacecraft will be launched in late 1992 and will serve as the target vehicle. After the second COMET spacecraft has been launched in late 1994, the ARD demonstration will take place. The service module from the second COMET will serve as the chase vehicle.

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