... of the proposed method. Wanyue Jiang is the corresponding author and can be contacted at: jwy1992@126.com 29 06 2017 09 12 2017 12 12 2017 07 01 2018 © Emerald Publishing Limited 2018 Emerald Publishing Limited Licensed re-use rights only Flight control Nash bargain...

...-TIFNN and CASMC. Flight control Performance Intelligent control Micro aircraft vehicle Attitude stabilization High pointing accuracy (Equation 7) (Equation 8) Next, propose x=bT, (Inline Equation 9) , the control model turned to as following eventually...

... to Equation (3). Attitude control of reusable launch vehicle (RLV) in reentry phase represents the lowest layer of reentry flight control among the three typical hierarchical levels: trajectory, guidance, and attitude control. The objective of attitude control is to realize the guidance commands so...

.... © Emerald Group Publishing Limited 2013 Flight control Nonlinear control Real-time systems Robust control Variable structure control During reentry, flight control systems of reentry vehicles operate over a large flight envelop. The reentry vehicles enter the atmosphere at high...

...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...

.... Originality/value The proposed control strategy is implemented on the helicopter and flight tests clearly demonstrate that a much better performance could be achieved, compared with convenient SMC schemes. © Emerald Group Publishing Limited 2012 Unmanned aircraft Approaching speed Flight control...

...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...

...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...

...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...

... 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...