Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1987-10-28
1988-04-05
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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.
Bush Freddie M.
Garvin, Jr. John C.
Jordan Charles T.
The United States of America as represented by the Secretary of
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