π€ AI Summary
Addressing the robust interception challenge of adversarial UAVs under complex environments and abrupt target maneuvers, this paper proposes an integrated guidance-and-control framework based on Adaptive Twisting-Structure Sliding Mode Control (ATSMC). Leveraging a two-dimensional coupled dynamics and relative kinematics model, we design a zero-effort missβbased sliding surface and pioneer the application of ATSMC to UAV integrated guidance-control architecture. The method requires no prior knowledge of target acceleration and simultaneously mitigates strong nonlinearities, model uncertainties, external disturbances, and sudden target direction changes. Simulation results demonstrate significantly improved interception accuracy, along with stable, rapid, and robust convergence even under high uncertainty and aggressive target maneuvers. This work establishes a novel paradigm for autonomous intelligent air combat interception.
π Abstract
This paper investigates an adaptive sliding-mode control for an integrated UAV autopilot and guidance system. First, a two-dimensional mathematical model of the system is derived by considering the incorporated lateral dynamics and relative kinematics of the UAV and its potential target of attack. Then, a sliding surface is derived utilizing the zero-effort miss distance. An adaptive twisting sliding mode (ATSMC) algorithm is applied to the integrated system. Simulation and comparisons have been accomplished. The results show our proposed design performs well in interception precision, even with high nonlinearity, uncertainties, disturbances, and abrupt changes in the target's movement, thanks to the adaptation strategy.