Remote reconnaissance and strike system and method based on multi-rotor unmanned aerial vehicle

• Main Authors: XU CHANGCHUN, GAI SHUAI, YAN KAI, JIA TAO, SUN BINGHAN, LI HAO
• Format: Patent
• Language: Chinese; English
• Published: 30.05.2023
• Subjects: AEROPLANES; AIRCRAFT; ALARM SYSTEMS; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; BLASTING; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; ELECTRIC COMMUNICATION TECHNIQUE; ELECTRICITY; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; HEATING; HELICOPTERS; LIGHTING; MECHANICAL ENGINEERING; ORDER TELEGRAPHS; PARACHUTES; PERFORMING OPERATIONS; PHYSICS; PICTORIAL COMMUNICATION, e.g. TELEVISION; SIGNALLING; SIGNALLING OR CALLING SYSTEMS; TRANSPORTING; WEAPONS; WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE ORCOMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR; WIRELESS COMMUNICATIONS NETWORKS

The invention discloses a remote reconnaissance and strike system based on a multi-rotor unmanned aerial vehicle and a reconnaissance and strike method, and belongs to the technical field of aviation systems. The method is characterized by specifically comprising a load integrated design, a multi-load control method, a multi-path image return method, a gun-mounted safety device design and a gun-mounted remote firing device design. According to the invention, the multi-rotor unmanned aerial vehicle carries multiple loads and weapon hangers to execute tasks; multi-load control and multi-path image return are realized through ground software and a signal adapter plate, application expansion aiming at a single-load control channel and a single-image channel link is realized, and integration of multiple functions of reconnaissance, strike and expelling of the multi-rotor unmanned aerial vehicle is realized; a safety device and a remote percussion device are designed for the structure of the firearm, and the multi-