Method and apparatus for determining close approaches for earth-

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

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244176, B64G 110

Patent

active

061023345

ABSTRACT:
Determining suitable launch windows to avoid or minimize close approaches between a launch vehicle and orbiting objects. A method and apparatus is disclosed for minimizing close approaches between spacecraft and other objects in space during the launch and early deployment phase of their lifetime, by defining a launch window, utilizing filters to screen certain objects in space from consideration and identifying launch window blackout times to avoid close approaches with the remaining objects in space under consideration.

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