Lateral acceleration control method for missile and corresponding weapon systems
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United States of America Patent
Stats
-
Aug 14, 1984
Grant Date -
N/A
app pub date -
Mar 26, 1982
filing date -
Apr 1, 1981
priority date (Note) -
Expired
status (Latency Note)
Importance
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.
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