Lateral acceleration control method for missile and correspondin

Details Lateral acceleration control method for missile and correspondin Lateral acceleration control method for missile and correspondin

1982-03-26

1984-08-14

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

044652496

ABSTRACT:
A lateral acceleration control method for a missile permits short response times to commands even of great amplitude. It comprises the association of an aerodynamic control system having large lateral acceleration capability, called PAF, with a force control system close to the center of gravity, having a moderate lateral acceleration capability, but with very short response time, called PIF. The overall response to a command includes the usual response of the aerodynamic automatic pilot to which there is added the response from the force control system, such that in the presence of a constant order, after a delay equal to the response time of the PAF, the PIF is entirely available for a new action.

REFERENCES:
patent: 3072365 (1963-01-01), Linscott et al.
patent: 3695555 (1972-10-01), Chadwick
patent: 3735944 (1973-05-01), Bannett et al.
patent: 4198015 (1980-04-01), Yates et al.
patent: 4277038 (1981-07-01), Yates et al.

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