A flight control system use in relation to an aviation vehicle having a thrust vectoring device for producing thrust, an air deflecting device for producing thrust having a box structure, and a computing system for receiving operation requirements is used to orient the thrust device and/or air defle
A flight control system use in relation to an aviation vehicle having a thrust vectoring device for producing thrust, an air deflecting device for producing thrust having a box structure, and a computing system for receiving operation requirements is used to orient the thrust device and/or air deflecting device.
대표청구항▼
1. A flight management system, use in relation to an aviation vehicle, comprising a thrust vectoring device for producing thrust, having a nozzle, a pivoting half cylinder side, a pivoting sphere with an inner-threaded aperture, a rotation pin, a passageway, a centered main panel slot, a deployment
1. A flight management system, use in relation to an aviation vehicle, comprising a thrust vectoring device for producing thrust, having a nozzle, a pivoting half cylinder side, a pivoting sphere with an inner-threaded aperture, a rotation pin, a passageway, a centered main panel slot, a deployment device, a threaded rod, an outer triangular panel with cut-out, a support means, a continuous hinge, a pivoting hydraulic cylinder, and a triangular main panel,an air deflecting device for producing thrust, having an open-ended box structure, a box securing plate, a motor shaft, a motor, a motor mount, a flat disc base, a support roller, and a rubber seal, anda computing system having storage storing machine-executable instructions configured for execution by the computing system in order to cause the computing system to receive operation requirements, the operation requirements used to orient the thrust device and/or the air deflecting device. 2. The system of claim 1 wherein the thrust vectoring device decreases the speed of the aviation vehicle. 3. The system of claim 1 wherein the air deflecting device further comprises a diagonal cross-brace. 4. The system of claim 1 wherein said pivoting half cylinder side rotates between a first position and a second position. 5. The system of claim 4 wherein the rotation of the pivoting half cylinder side is initiated by actuating the deployment device.
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