A Control System Surrounding the Surveillance and Fighting Integrated Aircraft

A control system and fire control system technology, applied in the field of reconnaissance and combat aircraft, can solve problems such as limited weapon launch angles, achieve the effects of concealed functions, large potential for weapons storage, and improved combat performance

Active Publication Date: 2021-03-19
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 problems of reconnaissance and strike fee reduction, the limited launch angle of weapons, etc., so as to realize reconnaissance and strike around and give it corresponding performance

Method used

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  • A Control System Surrounding the Surveillance and Fighting Integrated Aircraft
  • A Control System Surrounding the Surveillance and Fighting Integrated Aircraft
  • A Control System Surrounding the Surveillance and Fighting Integrated Aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

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

[0056] A co-pilot aircraft that surrounds, reconnaissance and strikes an integrated aircraft with a single-wing and double-launch layout. The front three-point landing gear and the main landing gear are 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-ground missile, with an airdrop drone mounted 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 navigable category II or III airport or highway about 500km away from the battlefield. Daily execution of single / dual aircraft surveillance missions and training, data link information is transmitted to the frontline headquarters. After receiving the combat task of intercepting the helicopter group...

Embodiment 2

[0057] Embodiment 2, applied to identification and verification at sea:

[0058] Ditto for aircraft. The loaded weapons are air-to-air missiles or air-to-surface missiles, the number is half and half. It is also loaded with 1 air-drop drone mounted under the belly of the machine. Equipped with electronic signal + electronic interference detection kit. Take off and land from island airports or inland airports to perform maritime patrol missions. According to the guidance of electronic signals, it arrives at an unknown ship near the sea, drops an air-dropped drone 50km away from the ship, carries optical reconnaissance equipment, and arrives at the ship to perform identification tasks. This aircraft is in standby flight according to the horizontal figure-of-eight route (such as Figure 11 As shown), keep shooting at the ship continuously, and execute the crew communication mode at the same time. After intercepting the electronic jamming signal emitted by the opposing ship, t...

Embodiment 3

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

[0060] Ditto for aircraft. Remove the weapons and equipment, and use the space of the aircraft fuselage 1 for aerial surveying and mapping, aerial prospecting, sea rescue airdrops, and express freight. Among them, when performing aerial prospecting flights on hilly terrain, the flight altitude is about 100-120m, and the abnormal aerodynamic configuration of the aircraft is used to provide compound changes in flight parameters, so as to obtain agile terrain-following flight control capabilities and improve the quality of prospecting. When performing sea rescue, the airborne optical pod finds the target point of the maritime accident, uses laser or calculation to locate the target point in time, lowers the altitude and returns to the accident site, and releases 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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Patent Type & Authority Patents(China)
IPC IPC(8): B64D7/00B64D47/00
CPCB64D7/00B64D47/00
Inventor 陶文英
Owner 陶文英
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