Adaptive Twisting Sliding Control for Integrated Attack UAV's Autopilot and Guidance
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 miss–based 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.