Burn Phase Corrections of Maneuver Ballistic Missiles with Star Light
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
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In this paper, the maneuver ballistic missile parametric correction in the burning phase with star light is studied, when the maneuver ballistic missile is launched under the condition that the initial position is not exactly defined and the inertial navigation platform is not completely leveled and aligned.
- Guided Missiles
- Space Navigation and Guidance