Dual-control scheme for improved missile maneuverability
AssigneeLockheed Martin Corporation
InventorWayne K. Schroeder
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AssigneeLockheed Martin Corporation
InventorWayne K. Schroeder
Estimating the term…
A comparative dual-control strategy actuates forward and aft control devices simultaneously to significantly improve a missile's maneuverability/dynamic capability. A substantial, and measurable, operational effect of the inventive control strategy is a dramatic improvement in a missile's divert capability. To effect a maneuver in accordance with the inventive strategy, a missile's aft fins are initially deflected to generate a force OPPOSITE that conventionally used (pushing the missile's tail in the direction of the commanded maneuver) which simultaneously actuating forward thrusters to also push the missile's nose in the direction of the commanded maneuver but at a faster rate than the tail section. This causes the missile body to simultaneously rotate and translate in the direction of the commanded maneuver. Once a sufficient amount of aerodynamic force develops due to body rotation, the aft fins are deflected to generate a force that opposes the commanded maneuver to maintain a moment on the missile body and complete the commanded maneuver. An important benefit of cooperative dual-control strategy is that the missile begins to translate in the direction of the commanded maneuver immediately (conventional isolated aft control schemes do not accomplish this) and at a faster rate than is possible with either isolated forward control devices or an intuitive dual-control approach.
A method for rapidly changing the direction of travel of a missile moving in a fluid medium to a desired new direction, said new direction being measured in the missile's inertial frame of reference, said missile having (i) a forward portion and a forward thruster control device and (ii) an aft portion and an aft fin control device, said method comprising:
A method for rapidly changing the direction of travel of a vehicle moving in a fluid medium to a desired new direction, said new direction being measured in the vehicle's inertial frame of reference, said vehicle having (i) a forward portion and a forward control device and (ii) an aft portion and an aft control device, said method comprising:
A control system for a vehicle having a forward portion referred to as a nose and an aft portion referred to as a tail, said system comprising:
A control system for a missile having a nose and a tail, said system comprising:
A method of maneuvering a vehicle, moving in a fluid medium, toward a direction of a commanded maneuver, said vehicle having:
A method for maneuvering a vehicle, moving in a fluid medium, toward a direction of a commanded maneuver, said vehicle having:
A control system for maneuvering a vehicle having a forward portion and an aft portion toward a direction of a commanded maneuver, said control system comprising:
A control system for maneuvering a vehicle having a forward portion and an aft portion toward a direction of a commanded maneuver, said control system comprising:
A memory device for use with an autopilot controller for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
A memory device for use with an autopilot controller for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
A method for generating control signals suitable for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
A method for generating control signals suitable for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
An autopilot controller for generating control signals suitable for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
An autopilot controller for generating control signals suitable for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having:
A memory device for generating control signals suitable for use with an autopilot controller for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having
A memory device for generating control signals suitable for use with an autopilot controller for maneuvering a vehicle toward a direction of a commanded maneuver, said vehicle having
A method for maneuvering a vehicle, moving in a fluid medium, toward a direction of a commanded maneuver, said vehicle having:
A control system for maneuvering a vehicle having a forward portion and an aft portion toward a direction of a commanded maneuver, said control system comprising:
A method for maneuvering a vehicle, moving in a fluid medium, toward a direction of a commanded maneuver, said vehicle having:
A control system for maneuvering a vehicle having a forward portion and an aft portion toward a direction of a commanded maneuver, said control system comprising:
Dependencies are inferred from the claim text.