2026· Proceedings of the 1st International Conference on Advanced Computation, Engineering Intelligence and Information Processing· pp. 24-30· 0 citations· 9 references
Abstract
: This article focuses on the use of drones to deploy smoke bombs in complex scenarios to deal with incoming missiles, aiming to design an optimal deployment strategy to maximize the effective shielding time of targets. This article first considers fixed parameters such as drone flight speed, direction, smoke bomb deployment, and detonation time. On this basis, precise motion trajectory models for missiles, drones, and smoke bombs were established. Secondly, the geometric judgment criteria for "line of sight obstruction" and the consideration of the 20 second effective time of the smoke screen have been added. At the same time, a complete numerical integration model for the duration of occlusion was established. By numerical solution, the effective masking time under this strategy is determined to be 1.4190s. Then, the flight speed, direction, deployment time, and detonation delay of the drone are used as decision variables to establish a parameterized dynamic trajectory model related to the decision variables, and constraints such as the range of drone flight speed are considered. Finally, the simulated annealing algorithm was used to solve the problem, and the maximum effective shielding time obtained was 4.7500 seconds. With the independent deployment and detonation time of three smoke bombs under a single flight strategy as the core decision variables, a dynamic system was established to describe the spatiotemporal trajectories of the three smoke clouds. Secondly, the ideas of "deployment interval not less than 1 second" and "maximizing the sum of shielding time" were added, ultimately establishing a complete multi-dimensional constraint optimization model.
In dynamic electro-optical confrontation environments that require real-time target concealment, ensuring the coordinated control of multiple obscuration agents remains a challenging problem in modern control systems. Especially under visiblelight reconnaissance, infrared imaging, and laser ranging or guidance conditio...
Yao-Hua Feng, Qian-Cheng Li, Zhi-Hao Xue· European Conference on Elect...· 0 citations
In view of the problems such as unstable attitude, hovering deviation, and reduced operational accuracy of fire-fighting drones caused by the superposition of multi-source disturbances such as high-temperature thermal plume and strong turbulence at the fire scene, this paper systematically reviews the relevant technolo...
Hao-Yu Yang· MATEC Web of Conferences· 0 citations
Flight safety is undoubtedly the core consideration in the trajectory planning of unmanned aerial vehicles (UAVs) during military missions. In light of this, how to comprehensively integrate flight data such as trajectory and flight speed, as well as the characteristics and performance of detectors in the mission envir...
Yuan-Wen Chen, Wei Xu, Shuang-Chao Xu et al.· International Conference on...· 0 citations
This paper studies smoke-munition release control for unmanned aerial vehicles in a reproducible three-dimensional simulation environment. The simulator integrates constant-altitude UAV flight, free-fall munition dynamics, post-detonation smoke-cloud settling, incoming-object motion, and a strict line-of-sight obscurat...
Yang Li, Hong-Yue Guo, Zhen-Yong An et al.· International Conference on...· 0 citations
This study examines how multiple uncrewed aerial vehicles (UAVs) should allocate tasks and coordinate smoke deployment to interrupt line of sight under fast, spatially dispersed incoming threats. A three-dimensional simulation framework is developed that couples proportional-navigation-like reference threat motion, aer...
Zhuo Tan, Di Wu, Yi Peng et al.· IEEE Access· 0 citations
With the increasing scale and density of low-altitude unmanned aerial vehicle (UAV) operations, safety separation between multirotor UAVs has become a critical parameter for low-altitude airspace management. Existing studies mainly consider aircraft geometry, navigation errors, trajectory deviations, and conventional c...