Publication Date:
2019-06-27
Description:
Computer program calculates trajectories of orbiting spacecraft and lander vehicles simultaneously. Using data from both vehicles, program calculates communications geometry which consists of orbiting spacecraft cone/clock angle, lander cone/clock angle, range, range rate and acceleration, and fade, reflective, and system margins.
Keywords:
MATHEMATICS AND INFORMATION SCIENCES
Type:
LAR-10658
Format:
application/pdf
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