Ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control

A technology of adaptive control and model reference, which is applied in the field of aerospace control and can solve problems such as poor real-time performance, high hardware requirements, and complex systems.

Inactive Publication Date: 2017-01-04
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, there is no public application report of the automatic landing system (ACLS) suitable for UAVs
[0005] To sum up, it can be seen that the existing automatic landing control technology for carrier-based aircraft generally has defects such as complex system, poor real-time performance, and high hardware requirements.

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  • Ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control
  • Ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control
  • Ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control

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Embodiment Construction

[0069] The technical scheme of the present invention is described in detail below in conjunction with accompanying drawing:

[0070] The principle of the shipboard UAV automatic landing control device based on model reference adaptive control in the present invention is as follows: figure 1 As shown in , it consists of two parts: landing command and glide reference trajectory generation module, and adaptive flight control module.

[0071] Landing command and glide reference trajectory generation module

[0072] The input signal of this module includes: the azimuth angle (ψ S +λ ac ), where ψ S is the azimuth angle of the ship, λ ac is the included angle of the inclined deck.

[0073] The output signal of this module includes the three-dimensional glide reference trajectory signal X EATDc (t), Y EATDc (t), Z EATDc (t) and speed command signal V c . Wherein, the glide reference trajectory signal and the speed command signal are output to the adaptive flight control mod...

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Abstract

The invention discloses a ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control, and belongs to the technical field of control of spacecraft instrumentation. The device comprises a ship landing command and gliding reference track generating module and a model reference adaptive flight control module, wherein the ship landing command and gliding reference track generating module is used for generating a three-dimensional gliding reference track signal and a speed command signal according to information of relative positions and absolute positions of a ship and a ship-borne unmanned aerial vehicle; and the model reference adaptive flight control module generates a flight control signal of the ship-borne unmanned aerial vehicle by a model reference adaptive control algorithm, so that an actual flight track and speed tracking ship landing command of the ship-borne unmanned aerial vehicle is the same as a three-dimensional gliding reference track signal and speed command generated by the gliding reference track generating module. The ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control is suitable for ship-borne manned aerial vehicles with fixed rings and ship-borne unmanned aerial vehicles with fixed rings. Compared with the prior art, the ship-borne unmanned aerial vehicle automatic ship landing control device based on model reference adaptive control does not need computation of a leading law; and ship landing is controlled accurately, a control system is simple, and control instantaneity is good.

Description

technical field [0001] The invention relates to an automatic landing control device for a ship-borne unmanned aerial vehicle based on model reference adaptive control, and belongs to the technical field of aerospace control. Background technique [0002] The "landing" in the present invention includes landing methods such as runway arrest landing, net collision recovery, etc., and has universality in the principle of the control method. [0003] As an important weapon force of the aircraft carrier, the key technology of carrier-based aircraft is how to ensure safe and accurate landing in a very harsh environment. Due to the harsh landing environment, disturbances such as mothership movement and ship tail airflow will have a great impact on UAV landing, which greatly increases the difficulty of carrier-based aircraft landing and seriously affects the safety of landing. During the sailing process of the ship, due to the influence of waves, sea surges and wind, the hull will p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B13/04G05D1/08G05D1/10
CPCG05B13/042G05D1/0808G05D1/101
Inventor 甄子洋王新华杨一栋
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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