... of the proposed method. Flight control Nash bargain Unmanned aerial vehicle The formation flight of unmanned aerial vehicles (UAVs) has received considerable interest in recent years. UAV formation flight has the advantages of high task efficiency, low cost, no casualties, etc. UAV rendezvous...

... initial rule positions for subsequent parameter learning. Furthermore, the structure and parameter adjustment are performed simultaneously. © Emerald Group Publishing Limited 2014 Flight control Performance Intelligent control Micro aircraft vehicle Attitude stabilization High...

... an appropriate control torque command vector M and then map the control torque command vector M to the aerodynamic surface deflection vector δ according to Equation (3). © Emerald Group Publishing Limited 2014 Flight control Nonlinear control Finite-time convergence...

... second order sliding mode is established, which implies that the closed-loop system is global robust against matched parameter uncertainties and disturbances in reentry. Second, the chattering problem is significantly alleviated. © Emerald Group Publishing Limited 2013 Flight control...

...Xun Gong; Yue Bai; Zhicheng Hou; Changjun Zhao; Yantao Tian; Qiang Sun Purpose The quad‐rotor is an under‐actuation, strong coupled nonlinear system with parameters uncertainty, unmodeled disturbance and drive capability boundedness. The purpose of the paper is to design a flight control system...

...Yang Gao; Jan Peters; Antonios Tsourdos; Yueheng Qiu; Weiguo Zhang; Xiaoxiong Liu; Pengxuan Zhao Purpose The purpose of this paper is to present the research into fault detection and isolation (FDI) and evaluation of the reduction of performance after failures occurred in the flight control system...

..., there exists N_1i(x_{i)=N1i+. Unmanned aircraft Approaching speed Flight control Sliding mode control Helicopters Chattering Sling mode control (SMC) has long been recognized as a robust method against uncertainty}...

...Yong Tian; Tian Li Purpose The purpose of this paper is to develop a novel type of full‐size flight control iron bird based on a passive electronic hydraulic servo loading system. Design/methodology/approach On the basis of mathematical modeling of passive loading system math model...

...Huangzhong Pu; Ziyang Zhen; Daobo Wang Purpose Attitude control of unmanned aerial vehicle (UAV) is the purposeful manipulation of controllable external forces to establish a desired attitude, which is inner‐loop of the autonomous flight control system. In the practical applications, classical...

... of the research work, mentioned in van Breugel et al. (2006) , is to evolve effective flight control patterns for a simulated physical ornithopter (with wing span of 1‐2 m) in terms of brazier curves, followed by partially evolving mechanical structures that would aid in the buildable ornithopters...