AN APPROXIMATE METHOD FOR COMPUTING ERROR COEFFICIENT MATRICES FOR LUNAR TRAJECTORIES
Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
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Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
Correction of space trajectories by small midcourse maneuvers governed by impulse which is computed on the ground from radio measurements and sent by radio to the space probe
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Computation of transition matrices or error coefficients in midcourse guidance studies of lunar trajectories
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