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Distributed optimisation approach to least-squares solution of Sylvester equations 期刊论文
IET CONTROL THEORY AND APPLICATIONS, 2020, 卷号: 14, 期号: 18, 页码: 2968-2976
作者:  Deng, Wen;  Zeng, Xianlin;  Hong, Yiguang
收藏  |  浏览/下载：147/0  |  提交时间：2021/01/14
least squares approximations  distributed control  stability  distributed algorithms  continuous time systems  matrix algebra  convex programming  multi-robot systems  convex optimisation  distributed optimisation approach  least-squares solution  Sylvester equations  distributed algorithms  multiagent network  problem setup  interconnected system  local information  data matrices  neighbour agents  continuous-time algorithms  optimisation problem  
Distributed optimisation design for solving the Stein equation with constraints 期刊论文
IET CONTROL THEORY AND APPLICATIONS, 2019, 卷号: 13, 期号: 15, 页码: 2492-2499
作者:  Chen, Guanpu;  Zeng, Xianlin;  Hong, Yiguang
收藏  |  浏览/下载：154/0  |  提交时间：2020/05/24
least squares approximations  gradient methods  convergence  matrix algebra  concave programming  multi-agent systems  distributed optimisation design  Stein equations  set constraints  rows  columns  coefficient matrices  equivalent distributed optimisation problem  projection-based algorithm  least-squares solution  constrained Stein equation  multiagent system network  simplified distributed algorithm  
On-line aerodynamic identification of quadrotor and its application to tracking control 期刊论文
IET CONTROL THEORY AND APPLICATIONS, 2017, 卷号: 11, 期号: 17, 页码: 3097-3106
作者:  Lei, Wenchao;  Li, Chanying
收藏  |  浏览/下载：193/0  |  提交时间：2018/07/30
helicopters  autonomous aerial vehicles  mobile robots  trajectory control  compensation  nonlinear control systems  discrete time systems  aerodynamics  online aerodynamic identification  quadrotor  tracking control  aerodynamic effects  quadrotor-type unmanned aerial vehicles  recursive least squares algorithm  aerodynamic parameters  accelerometer  nonlinear discrete-time trajectory tracking controllers  aerodynamic compensation  large-acceleration flight regime