ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Integrated design of high altitude super long endurance UAV system driven by distributed ground microwave power
Received date: 2023-12-14
Revised date: 2024-02-19
Accepted date: 2024-03-14
Online published: 2024-04-08
Supported by
National Natural Science Foundation of China(12202363)
High altitude super long endurance UAVs have important application values in the fields of wide view reconnaissance, communication relay, emergency rescue, etc. To achieve true super long endurance flight, a high-altitude unmanned flight system based on ground distributed launched microwave energy devices is proposed by utilizing the advantages of long-range transmission and low attenuation of 5.8 GHz microwave. The flight system mainly includes the flight part (rectenna), distributed transmission part, and high-precision guidance and tracking system for the interconnection of heaven and earth. The rectenna adopts a microstrip patch antenna fed by coplanar waveguides. The receiving antenna and rectifier circuit are put on the two sides of a layer of dielectric substrate. The rectifier circuit is optimized based on a direct through filter of a coplanar wave-guide, forming a circularly polarized rectifier array. The conversion efficiency of microwave to direct current is simulated to exceed 50%. The rectenna is fused with the body of the UAV in an approximate composite sandwich structure, forming a replaceable circular antenna area in the flat area of the lower part of the body. An after-loaded airfoil with a flat lower surface is used in this wingbody-rectenna region, and an optimized high-lift airfoil is applied in the outer sections of the UAV to ensure the overall efficiency of the UAV. The microwave launched antenna adopts a distributed transmitting array that is divided into several single parts and driven by servo systems to track the flight platform, and composites a microwave coverage area at the altitude of 18 km. The simulation data show that the beam collection efficiency of the launched system can reach up to 80%. The tracking guidance system also uses the distributed locating strategy, which can achieve ultra-high precision location of the UAV with an altitude of 30 m by combining with the extended Kalman filtering algorithm. A 1∶6.7 scaled model is designed to test the developed system. The scaled UAV with rectenna arrays flies through the microwave coverage area generated by a single ground launched antenna with 80 W total power, and the rectenna successfully achieves and transmits the power of the microwave at an altitude of 8 m, which indicates the feasibility of the system proposed.
Baigang MI , Hao ZHAN , Liwei SONG , Guodong QIN , Yangping DENG . Integrated design of high altitude super long endurance UAV system driven by distributed ground microwave power[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(17) : 529982 -529982 . DOI: 10.7527/S1000-6893.2023.29982
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