Mode-transition control law design for aircraft with ability of VTOL and high-speed cruise flight
Penghui Fan , Chenxi Zhang , Xinhua Wang , Kaiyuan Cai
chinese control conference 3284 -3289
2
2010
Hardware Implementations with High Throughput, Low-Latency and Low-Area for Matrix Inversion
Yiqun Zhu , Qizhi Shi , Xinhua Wang , Xiaolin Meng
field programmable technology 250 -255
1
2020
Nonlinear continuous integral-derivative observer
Xinhua Wang , Bijan Shirinzadeh
Nonlinear Dynamics 77 ( 3) 793 -806
8
2014
Nonlinear Signal-Correction Observer and Application to UAV Navigation
Xinhua Wang , Weicheng Wang
IEEE Transactions on Industrial Electronics 66 ( 6) 4600 -4607
7
2019
Periodic Orbit Analysis of Switched Linear Systems
Jing-Ya Su , Xinhua Wang , Kai-Yuan Cai
international conference on automation and logistics 1425 -1430
2007
Finite-Time-Convergent Differentiator Based on Singular Perturbation Technique
Xinhua Wang , Zengqiang Chen , Geng Yang ,
IEEE Transactions on Automatic Control 52 ( 9) 1731 -1737
105
2007
Rapid-convergent nonlinear differentiator
Xinhua Wang , Bijan Shirinzadeh
Mechanical Systems and Signal Processing 28 414 -431
23
2012
High-order nonlinear differentiator and application to aircraft control
Xinhua Wang , Bijan Shirinzadeh
Mechanical Systems and Signal Processing 46 ( 2) 227 -252
34
2014
Nonlinear augmented observer design and application to quadrotor aircraft
Xinhua Wang , Bijan Shirinzadeh
Nonlinear Dynamics 80 ( 3) 1463 -1481
25
2015
Design and control for rotor-fixed wing hybrid aircraft:
Xinhua Wang , Hai Lin
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 225 ( 7) 831 -847
11
2011
Equivalent Sliding Mode Control Based On Nonlinear Observer For Nonlinear Non-Minimum-Phase Systems
Xinhua Wang , Geng Yang
Journal of Dynamical and Control Systems 13 ( 1) 25 -36
2
2007
Tracking control for VTOL aircraft with disabled IMUs
Xinhua Wang , Jinkun Liu , Kai-Yuan Cai
International Journal of Systems Science 41 ( 10) 1231 -1239
8
2010
Output tracking for nonlinear non-minimum phase systems with output delay and application to an F-16 jet fighter
Bo Zhu , Xinhua Wang , Kai-Yuan Cai
International Journal of Systems Science 42 ( 3) 529 -538
15
2011
Aircraft navigation based on differentiation–integration observer
Xinhua Wang , Lilong Cai
Aerospace Science and Technology 68 109 -122
2
2017
Navigation and Control Based on Integral-Uncertainty Observer for Unmanned Jet Aircraft
Lilong Cai , Xinhua Wang
IEEE Transactions on Aerospace and Electronic Systems 53 ( 3) 1230 -1249
2
2017
Nonlinear Multiple Integrator and Application to Aircraft Navigation
Xinhua Wang , Bijan Shirinzadeh
IEEE Transactions on Aerospace and Electronic Systems 50 ( 1) 607 -622
22
2014
Nonlinear Double-Integral Observer and Application to Quadrotor Aircraft
Xinhua Wang , Bijan Shirinzadeh , Marcelo H. Ang
IEEE Transactions on Industrial Electronics 62 ( 2) 1189 -1200
68
2015
Takeoff/landing control based on acceleration measurements for VTOL aircraft
Xinhua Wang
Journal of The Franklin Institute-engineering and Applied Mathematics 350 ( 10) 3045 -3063
8
2013
Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft
Xinhua Wang , Geng Yang , Wenli Xu
International Journal of Systems Science 39 ( 1) 29 -42
9
2008
Design and frequency analysis of continuous finite-time-convergent differentiator
Xinhua Wang , Hai Lin
Aerospace Science and Technology 18 ( 1) 69 -78
32
2012