12 June 1995 Improved video guidance sensor for automated docking
Author Affiliations +
The Video Guidance Sensor (VGS) has been developed by NASA's Marshall Space Flight Center (MSFC) to provide the capability for a spacecraft to find and track a target vehicle and determine the relative positions and attitudes between the sensor and the target. The sensor uses laser diodes to illuminate the target, a CCD-based camera to sense the target, and a frame-grabber and processor to convert the video information into relative range, azimuth, elevation, roll, pitch, and yaw. The sensor was first built in 1988 and used in successful automated docking experiments using the air-bearing spacecraft simulator in MSFC's Flight Robotics Laboratory. Since then, many changes and improvements have been made, based on the results of testing. In addition to the use of this system for space vehicles, it has been adapted for commercial application. The current design is being built as a prototype to prepare for flight testing on the Space Shuttle. Some of the changes from the original system were designed to improve the noise rejection of the system. Other changes were made to improve the overall range of operation of the system, and still other changes improved the bandwidth of the system. The current VGS is designed to operate from 110 meters down to 0.5 meters and output the relative position and attitude data at 5 Hz. The system will be able to operate under any orbital lighting conditions from full solar illumination to complete darkness. The VGS is also designed to be used with more than one target and sensor to allow for redundant configurations. This new prototype should be completed and undergoing open- and closed-loop testing after March 1995.
© (1995) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Richard T. Howard, Richard T. Howard, Michael L. Book, Michael L. Book, } "Improved video guidance sensor for automated docking", Proc. SPIE 2466, Space Guidance, Control, and Tracking II, (12 June 1995); doi: 10.1117/12.211499; https://doi.org/10.1117/12.211499


DART AVGS flight results
Proceedings of SPIE (May 02 2007)
Retroreflector Field Tracker
Proceedings of SPIE (November 07 1984)
Video guidance sensor flight experiment results
Proceedings of SPIE (September 07 1998)
Ground testing the Hydra AR&D sensor system
Proceedings of SPIE (April 14 2008)
Active sensor system for automatic rendezvous and docking
Proceedings of SPIE (August 05 1997)

Back to Top