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Minimax estimate of accuracy in determining a spacecraft orbit allowing for unmodeled accelerations
Minimax estimate of accuracy in determining a spacecraft orbit allowing for unmodeled accelerations
1979
V. A. Arkhangelskii
L. Iu. Belousov
Keywords:
Orbit
Mathematical optimization
Spacecraft
Celestial mechanics
Minimax
Trajectory optimization
Classical mechanics
Integral equation
Physics
Correction
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