The invention relates to a vertical take-off and landing unmanned plane lift augmentation control device and a vertical take-off and landing unmanned plane lift augmentation control method, and relates to a vertical take-off and landing unmanned plane. The control device is provided with foldable drive motors, foldable wing flaps, an oil amount sensor, a cargo dispensing amount sensor and a flight control system, wherein the foldable drive motors and the foldable wing flaps are arranged in compartments at two sides of wing body fused flying wings; the output end of the oil amount sensor and the output end of the cargo dispensing amount sensor are connected with the input end of the flight control system, the output end of the flight control system is connected with the foldable drive motor, and the oil amount sensor, the cargo dispensing amount sensor and the flight control system are arranged in the wing body fused flying wings. By adopting the vertical take-off and landing unmanned plane lift augmentation control device, an unmanned plane can vertically take off and land, hover, inversely fly and make spot turn, the mobility is good, and the requirement on the take-off and landing condition is relatively low; the cruising ability is strong, and the unmanned plane is suitable for the flight task with relatively high requirement for the flight hour; the unmanned plane is good in stability and is suitable for carrying an automatic driverscope, an airborne camera and a to-be-dispensed material resources; under a level flight state, the lift area can be adjusted along with the variation of the gravity.
Vertical take-off and landing unmanned plane lift augmentation control device and vertical take-off and landing unmanned plane lift augmentation control method
2015-05-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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|Composite lift force type unmanned aerial vehicle realizing vertical take-off and landing
European Patent Office | 2015
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