reflector navigation structure general satellite info ilrs support retroreflector info center of mass site performance info

RANGE: Reflector Information

RANGE LLR Location
RANGE Coordinate system
CCR enumeration
CCR orientation
CCR Occlusion diagram

Contact information:

Name: Brian Gunter
Organization and position: Georgia Institute of Technology, Assistant Professor
Address: School of Aerospace, 270 Ferst Drive NW, Atlanta, GA 30332-0150
Phone number: +1 404-385-2345
E-mail address: brian.gunter@aerospace.gatech.edu

Position (XYZ) of the center of the front face of each corner cube, and the orientation (two angles or normal vector) and the clocking (horizontal rotation) angle of each corner cube:

Position is (x, y, z) in mm from satellite fixed body frame, in mm. All vectors are (x, y, z) unit vectors in same frame.

Cube Position Orientation Normal Vector Clocking Vector
CCR1 (34.605, 17.886, 5.106) (0.259, 0.259, -0.930) (-0.643, 0.765, 0.034)
CCR2 (65.963, 18.076, 5.001) (-0.259, 0.259, -0.930) (-0.114, 0.949, 0.296)
CCR3 (65.963, 81.923, 5) (-0.259, -0.259, -0.930) (0.339, -0.927, 0.164)
CCR4 (34.605, 82.114, 5.106) (0.259, -0.259, -0.930) (0.615, -0.698, 0.366)
CCR5 (67.532, 110.842, 142.628) (0, 0.259, -0.966) (0, -0.966, -0.259)

 

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