Paper
23 September 1994 Dual-theodolite real-time computation method used during the optical alignment of the Excitation by Electron Deposition (EXCEDE) III rocket payload
David S. Akerstrom, Charles J. Galanis, Robert F. Stuart
Author Affiliations +
Abstract
Phillips Laboratory and Systems Integration Engineering developed a two-theodolite, reflecting-surface technique for measuring the lines of sight (LOS) of sensors in rocket payload modules. A flat mirror, keyed to one theodolite provides a stable and adjustable reference by which the angular separation of sensor LOS's can be measured and referenced to the rocket's coordinate system. The rocket's Attitude Control System and external launch pad geodetic survey points are referenced to the vehicle's geometry using this procedure.
© (1994) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
David S. Akerstrom, Charles J. Galanis, and Robert F. Stuart "Dual-theodolite real-time computation method used during the optical alignment of the Excitation by Electron Deposition (EXCEDE) III rocket payload", Proc. SPIE 2267, Advanced Microdevices and Space Science Sensors, (23 September 1994); https://doi.org/10.1117/12.187473
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KEYWORDS
Sensors

Mirrors

Rockets

Cameras

Optical alignment

System integration

Geodesy

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