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An automatic landing guidance method for shipborne UAV

An automatic landing and unmanned aerial vehicle technology, applied in the direction of aircraft automatic landing aids, etc., can solve the problems of poor engineering realization, increased system complexity and instability, and large amount of calculations

Inactive Publication Date: 2015-07-29
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0004] Conventional guidance algorithms, such as proportional guidance method and deviation elimination method, are almost limited by the dynamic changes of the target area. If the dynamic change prediction is not accurate, the guidance performance will be significantly reduced. In addition, the general intelligent guidance method still has a large amount of calculation. , The disadvantage of slow learning convergence speed, easy to increase the complexity and instability of the system, and poor engineering realization

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  • An automatic landing guidance method for shipborne UAV
  • An automatic landing guidance method for shipborne UAV
  • An automatic landing guidance method for shipborne UAV

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Embodiment Construction

[0052] Below in conjunction with accompanying drawing, the technical scheme of invention is described in detail:

[0053] The present invention relates to a ship-borne unmanned aerial vehicle automatic landing guidance method. The recovery method of the ship-borne unmanned aerial vehicle is collision net recovery, the unmanned aerial vehicle enters the field and lands at a constant speed, and the aircraft carrier sails in a straight line. For UAVs in any flying state, the process of guiding the carrier-based UAV to the landing point is divided into the capture phase and the tracking phase according to the different stages of its approach and landing, such as figure 1 As shown, in the capture phase, since the shipboard UAV is far away from the ship, the influence of deck movement on the flight track is not considered, and the shipboard UAV is guided from any flight state to the capture point p 0 (i.e. the apex of the glideslope), using the direct line-of-sight method. determin...

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Abstract

The invention discloses an automatic carrier-landing guiding method of a carrier-borne unmanned aircraft and belongs to the technical field of automatic carrier-landing guiding for carrier-borne aircrafts. The method comprises the following steps of determining a reference flight path at a capturing phase according to the initial course information and the positional information of the unmanned aircraft, determining a reference flight path at a tracking phase by considering the influence of deck movement, acquiring a flight-path error at the capturing phase by adopting a direct sightline method, and obtaining a flight-path error at the tracking phase by adopting a dynamic coordinate-system changing method; calculating longitudinal and transverse control-signal instruction values according to the flight-path errors, and guiding the carrier-borne unmanned aircraft to fly along the reference flight paths. The automatic carrier-landing guiding method of the carrier-borne unmanned aircraft provided by the invention has high realizability and operability, so that the carrier-landing performance of the unmanned aircraft under a specific carrier-landing environment is improved; the deck movement is directly led into a carrier-landing tracking-phase guiding algorithm, so that the addition of a deck-movement compensator to a controller is avoided, the complexity of a flight control system is lowered, and the reliability of a carrier-landing system is improved.

Description

technical field [0001] The invention discloses an automatic landing guidance method for a ship-borne unmanned aerial vehicle, which belongs to the technical field of automatic landing guidance for a ship-borne aircraft. Background technique [0002] Due to the broad application prospects of shipborne UAVs in future naval warfare, various naval powers have listed them as one of the important equipment for future large and medium-sized ships. At present, most shipboard UAVs use remote control equipment to ensure stability and controllability during the entire flight phase from takeoff to landing. With the continuous development of science and technology, naval powers require shipboard UAVs to be able to take off and land autonomously / automatically. Therefore, the research on UAV automatic landing technology is particularly important. Landing recovery. Since the research on shipborne UAVs is in its infancy, and due to reasons such as undisclosed technology, there are few publ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G08G5/02
Inventor 郑峰婴龚华军袁锁中戴文正甄子洋江驹王新华周鑫
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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