Method and system for controlling hover, reconnaissance and strike integrated aircraft

A control method and aircraft technology, applied in the field of reconnaissance and combat aircraft, can solve problems such as the limited launch angle of weapons, achieve concealment of functions, improve coordinated command and maneuver operations on the battlefield, and reduce aerodynamic resistance.

Active Publication Date: 2018-05-04
陶文英
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a control method and system for an integrated aircraft that surrounds reconnaissance and strikes, so that it can solve the p

Method used

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  • Method and system for controlling hover, reconnaissance and strike integrated aircraft
  • Method and system for controlling hover, reconnaissance and strike integrated aircraft
  • Method and system for controlling hover, reconnaissance and strike integrated aircraft

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0055] Embodiment 1, applied to low-altitude fixed-point interception:

[0056] A co-piloted aircraft, with a single-wing and double-release station, with the first three-point landing gear and the main landing gear retracted into the outer bulge of the fuselage. The flight ceiling is 7500m, the endurance time is 8h, and the load is about 1500kg. "Tianyan" PL90 air-to-air missile, or "Blue Sword" AKD10 air-to-surface missile, is equipped with an air-dropped UAV outside the belly, equipped with electronic signal + photoelectric pod detection kit. The aircraft is equipped by army special forces or army aviation. Take off / land at a general aviation Class II or III airport or highway about 500km from the battlefield. Perform daily single-machine / dual-machine surveillance tasks and training, and transmit data link information to the front-line command. After receiving the combat mission of intercepting the helicopter group, the two-plane installation was activated, and the ratio of ...

Example Embodiment

[0057] Embodiment 2, applied to maritime identification verification:

[0058] The aircraft is the same as above. The loaded weapons are air-to-air missiles, or air-to-surface missiles, and the number is divided into half. There is also 1 air-dropped drone under the belly of the loader. Equipped with electronic signal + electronic interference detection kit. Take off and land from island airports or inland airports to perform maritime inspection tasks. According to the guidance of electronic signals, it will arrive at an unknown ship at sea, and drop an air-dropped UAV at a distance of 50km from the ship, carrying optical reconnaissance equipment, and approach the ship to perform identification tasks. The aircraft will fly in standby mode on the horizontal 8-character route (e.g. Picture 11 (Shown), keep firing continuously on the ship, and execute the crew communication mode. After intercepting the electronic jamming signal from the other ship, the machine will approach the ...

Example Embodiment

[0059] Embodiment 3, the refitting and use of the integrated aircraft:

[0060] The aircraft is the same as above. The weapons and equipment are dismantled and used for aerial surveying and mapping, aerial prospecting, maritime rescue, airdrop, and express cargo with the help of the space of the aircraft fuselage 1. Among them, when performing aerial prospecting flight in hilly terrain, the flight altitude is about 100-120m. The abnormal aerodynamic configuration of the aircraft is used to provide compound changes of flight parameters, to obtain agile terrain following flight control capabilities, and to improve the quality of prospecting. When performing maritime rescue, the airborne optical pod found the target point of the maritime accident, and used laser or calculation to locate the target point in time, lowered the altitude and returned to the accident location, and dropped rescue items.

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PUM

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Abstract

The invention discloses a method and system for controlling hover, reconnaissance and strike integrated aircraft. The control system comprises aircraft, airborne weapon systems, airborne detection systems and a ground monitoring station; belly suspending plates are installed on the aircraft of all states and weapons are installed on the belly suspending plates, electro-optical pods can be installed and the lifting height of the electro-optical pods can be adjusted to prevent the firing of the weapons from being interfered, and other weapons can be suspended outside under wings or on a fuselagewhile the belly suspending plates are installed. According to the designing scheme of the method and system for controlling the hover, reconnaissance and strike integrated aircraft, the problem of limited weapon firing angle is solved, by arranging the belly suspending plates, missiles arranged on the suspending plates are capable of keeping in the same pointing direction with an observing and sighting device at any time, but synchronously alignment is not necessary, the missiles only need to be capable of keeping in the same pointing direction with the observing and sighting device at any time, or capable of pointing at the same direction along with the observing and sighting device, and therefore firing conditions can be set up at any time to overcome defects in the prior art.

Description

technical field [0001] The invention belongs to the reconnaissance and combat aircraft in the aviation field, in particular to a manned aircraft, a co-piloted aircraft and an unmanned aerial vehicle system with the integrated purpose of reconnaissance and strike. Background technique [0002] The active inspection and attack integrated drones are mainly unmanned aircraft, which can extend the function of inspection and attack integration to various manned aircraft and various unmanned aircraft, referred to as inspection and attack aircraft. Piloting a plane (ZL201510438906.6 A control method and system for cooperative piloting aircraft system for short) and unmanned aerial vehicle system, a standard unmanned aerial vehicle system cut from a joint piloting plane. [0003] The typical weapons of the integrated UAV are laser-guided missiles, guided bombs, etc. Mounting missiles under the wings is the most common layout, so the attack range of missiles is mainly the front hemis...

Claims

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Application Information

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IPC IPC(8): B64D7/00B64D47/00
CPCB64D7/00B64D47/00
Inventor 陶文英
Owner 陶文英
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