Distributed event triggering control for six-rotor UAV systems with asymmetric time-varying output constraints

被引:53
|
作者
Cao, Liang [1 ]
Ren, Hongru [1 ]
Meng, Wei [1 ]
Li, Hongyi [1 ]
Lu, Renquan [1 ]
机构
[1] Guangdong Univ Technol, Guangdong Prov Key Lab Intelligent Decis & Cooper, Guangzhou 510006, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
adaptive neural control; asymmetric time-varying output constraints; event triggering mechanism; input saturation; six-rotor UAV systems; TRAJECTORY TRACKING CONTROL; UNMANNED AERIAL VEHICLE; NONLINEAR-SYSTEMS; CONSENSUS CONTROL; ATTITUDE-CONTROL; DESIGN; DELAY; STATE;
D O I
10.1007/s11432-020-3128-2
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Inspired by the practical operability and safety of unmanned aerial vehicles (UAVs) in confined areas, this paper investigates adaptive trajectory tracking control problems in multiple six-rotor UAV systems with asymmetric time-varying output constraints and input saturation. Under model and disturbance uncertainties, six-rotor UAV systems are modeled as two non-strict-feedback systems, including attitude (inner-loop) and position (outer-loop) regulation systems. For the inner-loop design, the neural-based distributed adaptive attitude consensus control protocol is employed to realize the leader-follower consensus. Adaptive first-order sliding mode differentiators and an auxiliary dynamic system are introduced to address the "explosion of complexity" and saturation nonlinearity issues, respectively. Then, an event-triggered condition is predefined to alleviate the communication loads and reduce the number of messages to be transmitted from the controller to actuator. In addition, a class of asymmetric time-varying barrier Lyapunov functions are constructed for preventing the violation of time-varying output constraints. Accordingly, the proposed double-loop control strategies guarantee that all signals of UAV systems are semi-globally and uniformly bounded. Simulation results demonstrate that the proposed control method is effective.
引用
收藏
页数:16
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