Take-off and landing platform of air vehicle, control system, take-off method and landing method
A technology for a control system and aircraft, applied in the field of aircraft, can solve problems such as the inability to ensure the take-off or landing stability of unmanned helicopters, and achieve the effects of improving take-off stability, ensuring stability, and improving stability
Inactive Publication Date: 2017-06-16
SHANGHAI LIANGMING TECH DEV
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Problems solved by technology
At present, in order to facilitate the take-off and landing of unmanned helicopters, it is common to artificially select areas with relatively stable ground surfaces to carry unmanned helicopters during take-off and landing, and it is impossible to ensure the stability of take-off or landing of unmanned helicopters.
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[0047] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0048] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.
[0049] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but not as a limitation of the present invention.
[0050] Such as Figure 1-2 As shown, a landing platform of an aircraft is used to carry an aircraft 1, and the ...
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The invention provides a take-off and landing platform of an air vehicle, a control system, a take-off method and a landing method and belongs to the field of air vehicles. The take-off and landing platform of the air vehicle comprises a base plate for bearing the air vehicle, a second magnetic device arranged on the base plate and corresponding to the position of a first magnetic device of the air vehicle and identical to the first magnetic device in magnetism so as to make the first magnetic device pop up, a power supply unit connected with the second magnetic device and used for providing electric energy for the second magnetic device, and a control unit connected with the power supply unit and used for controlling the power supply unit to supply power for the second magnetic device. The take-off and landing platform can provide a push force for take-off of an unmanned helicopter and ensures the take-off and landing stability of the unmanned helicopter.
Description
technical field [0001] The invention relates to the field of aircraft. Background technique [0002] An unmanned helicopter (Unmanned Aerial Vehicle, UAV) refers to a flight device without a pilot in the aircraft, which can be controlled or automatically fly, and land in various environments to perform multiple tasks. [0003] Nowadays, the research and application of small unmanned helicopters are becoming more and more common, and they are widely used in surveillance, investigation, early warning, electronic countermeasures, communication relay and other military occasions, as well as environmental monitoring, aerial survey and aerial photography, weather forecasting, earthquake fire and other disaster search and rescue , inspection of transmission lines and railway lines and other civil occasions. Since UAVs do not need to consider human physiological and psychological endurance limits when designing, they can have higher maneuverability and flexibility. At present, in ...
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IPC IPC(8): B64F1/00B64F1/06
CPCB64F1/00B64F1/06
Inventor 马宇尘
Owner SHANGHAI LIANGMING TECH DEV