Tytuł artykułu

Comparative investigations of nonlinear and linear observers for a highly manoeuvrable target in sliding mode guidance

Tytuł czasopisma

Bulletin of the Polish Academy of Sciences Technical Sciences

Rocznik

2017

Wolumin

65

Numer

No 2

Autorzy

Wang, Y. ; Sun, M. ; Du, S. ; Chen, Z.

Wydział PAN

Nauki Techniczne

Zakres

233-245

Data

2017

Identyfikator

DOI: 10.1515/bpasts-2017-0027 ; ISSN 2300-1917

Źródło

Bulletin of the Polish Academy of Sciences: Technical Sciences; 2017; 65; No 2; 233-245

Referencje

Cho (2016), Optimality of augmented ideal proportional navigation for maneuvering target interception on Aerospace Electronic Systems, IEEE Trans, 52, 948. ; Wu (2016), Practical solution to efficient flight path control for hypersonic vehicle of the Japan Society for Aeronautical and Space Sciences, Trans, 59, 195. ; Przybyla (2012), Active disturbance rejection control of a DOF manipulator with significant modeling uncertainty, Bull Tech, 2, 509. ; Han (2009), From PID to active disturbance rejection control on Industrial Electronics, IEEE Trans, 56, 900. ; Angulo (2013), Robust exact uniformly convergent arbitrary order differentiator, Automatica, 49, 2489, doi.org/10.1016/j.automatica.2013.04.034 ; Qiu (2014), Practical wind disturbance rejection for large deep space observatory antenna on Control System Technology, IEEE Trans, 22, 1983. ; Levant (2009), Non - homogeneous finite - time - convergent differentiator on Decision and Control and Chinese Control Conf, IEEE Conf, 8399. ; Aguilera (2013), Singular linear parameter - varying observer for composition estimation in a binary distillation column Theory and Applications, IET Control, 7, 411, doi.org/10.1049/iet-cta.2011.0469 ; Bartolini (1998), Chattering avoidance by second - order sliding mode control on Automatic Control, IEEE Trans, 43, 241. ; Mokhtari (2006), Feedback linearization and linear observer for a quadrotor unmanned aerial vehicle, Advanced Robotics, 20, 71, doi.org/10.1163/156855306775275495 ; Shtessel (2009), Guidance and control of missile interceptor using second - order sliding modes on Aerospace Electronic Systems, IEEE Trans, 45, 110. ; Sun (2014), Practical solution to attitude control within wide envelope Aerospace Technology, Aircraft Engineering, 86, 117, doi.org/10.1108/AEAT-10-2012-0167 ; Wang (2015), Adaptive nonsingular terminal sliding mode guidance law against maneuvering targets with impact angle constraint of IMechE Part, Proc Aerospace Engineering, 229, 867. ; Levant (1998), Robust exact differentiation via sliding mode technique, Automatica, 34, 379, doi.org/10.1016/S0005-1098(97)00209-4 ; Kamal (2016), Continuous terminal sliding - mode controller, Automatica, 69. ; Lee (2007), Guidance law to control impact time and angle on Aerospace Electronic Systems, IEEE Trans, 43, 301. ; Shtessel (2007), Smooth second - order sliding modes : Missile guidance application, Automatica, 43, 1470, doi.org/10.1016/j.automatica.2007.01.008