Rate aided tracking for launch transient survivability

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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F41G 722

Patent

active

H00004553

ABSTRACT:
Rate aiding tracking prevents or dampens the effect of large scale target tion on a missile borne tracker during transition of a missile from prelaunch tracking to post launch tracking. Rate aided tracking includes a feedback network responsive to existing stable platforms for combining a tracker output signal with a rate signal that is itself responsive to torques present on a stable platform due to target sensor motion. The feedback network includes an integrator and a transformation circuit and is active only during the missile launching phase of operation when transient effects are manifest.

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