Abstract:Aiming to achieve a stable strip effect during rice aerial seeding and address the issue of safe unmanned aerial vehicle (UAV)take-off and landing caused by extending the seeding tube, a non-driven and gravity-based foldable seeding device was proposed. By analyzing the rice strip-seeding process based on UAV, it was determined that the inner diameter of the seeding tube, the ratio of tube length to UAV flight height (length-to-height ratio), and the configuration combination of the seeding tube influenced the degree of seed confinement, the disturbance intensity of ground diffusion airflow on seeds, and the stability of the UAV??s flight posture, thereby affecting the strip effect of seeds. Based on the 3WTYI6-20C six-rotor agricultural spraying UAV, a mud-box seeding test was conducted for optimization. Results indicated that when the tube??s inner diameter was 22 mm, the length-to-height ratio was 0. 714, and the configuration combination was Ⅳ, the seed confinement effect of the seeding tube was optimal, the UAV's flight posture remained stable, and the strip width reached 62. 1 mm with a strip index of 0. 75. Using these factor values, mud-box experiments were performed at operation speeds ranging from 1 m / s to 5 m / s. Results showed that for the 3WTYI6-20C six-rotor agricultural spraying UAV, the strip width ranged from 58. 3 mm to 69. 2 mm, and the strip index ranged from 0. 72 to 0. 77. Meanwhile, the 3WWDZ-60A four-rotor agricultural spraying UAV equipped with the non-driven and gravity-based foldable seeding device achieved a strip width range of 84. 5 mm to 92. 5 mm and a strip index range of 0. 63 to 0. 66, which demonstrated the stable strip effect. These findings suggest that the non-driven and gravity-based foldable seeding device can be effectively adapted to various UAV architectures and achieve stable rice strip-seeding effects across different operation speeds.