Paper
24 August 2010 Pointing performance of an aircraft-to-ground optical communications link
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Abstract
We present results of the acquisition and pointing system from successful aircraft-to-ground optical communication demonstrations performed at JPL and nearby at the Table Mountain Facility. Pointing acquisition was accomplished by first using a GPS/INS system to point the aircraft transceiver's beam at the ground station which was equipped with a wide-field camera for acquisition, then locking the ground station pointing to the aircraft's beam. Finally, the aircraft transceiver pointing was locked to the return beam from the ground. Before we began the design and construction of the pointing control system we obtained flight data of typical pointing disturbances on the target aircraft. We then used these data in simulations of the acquisition process and of closed-loop operation. These simulations were used to make design decisions. Excellent pointing performance was achieved in spite of the large disturbances on the aircraft by using a direct-drive brushless DC motor gimbal which provided both passive disturbance isolation and high pointing control loop bandwidth.
© (2010) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Martin W. Regehr, Abhijit Biswas, Joseph M. Kovalik, and Malcolm W. Wright "Pointing performance of an aircraft-to-ground optical communications link", Proc. SPIE 7814, Free-Space Laser Communications X, 781403 (24 August 2010); https://doi.org/10.1117/12.858632
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CITATIONS
Cited by 4 scholarly publications.
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KEYWORDS
Control systems

Transceivers

Device simulation

Control systems design

Sensors

Cameras

Interfaces

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