MATEC Web Conf.
Volume 214, 20182018 2nd International Conference on Information Processing and Control Engineering (ICIPCE 2018)
|Number of page(s)||5|
|Section||Electronic Information Technology and Control Engineering|
|Published online||15 October 2018|
- Bolender M A. An Overview on Dynamics and Controls Modelling of Hypersonic Vehicles. 2009 American Control Conference, pp.2507–2512. [Google Scholar]
- Wang Q, Stengel R F.Robust nonlinear control of a hypersonic aircraft.Journal of Guidance, Control and Dynamics, 2000, 23(4), pp.577–584. [CrossRef] [Google Scholar]
- ITO D, WARD D, VALASEK J. Robust dynamic inversion controller design and analysis for the X-38. AIAA Guidance, Navigation, and Control Conference. Montreal, Canada, 2001. [Google Scholar]
- Xu H J, Mirmirani M, Ioannou P A.Robust neural adaptive control of a hypersonic aircraft.AIAA Guidance, Navigation, and Control conference and Exhibit. Austin, Texas, 2003. [Google Scholar]
- Wallner E M, Well K H.Nonlinear flight control design for the X-38 using CMAC neural networks.AIAA Guidance, Navigation, and Control Conference and Exhibit. Montreal, Canada, 2001. [Google Scholar]
- Xu H J, Ioannou P A, Mirmirani M.Adaptive sliding mode control design for a hypersonic flight vehicle. Journal of Guidance, Control and Dynamics, 2004, 25(5), pp.829–838. [NASA ADS] [CrossRef] [Google Scholar]
- Junchun Yang, Jun Hu, Xiaole Lv.Design of Sliding Mode Tracking Control for Hypersonic Reentry Vehicles. Proceedings of the 26th Chinese Control Conference, Zhangjiajie, Hunan, China, 2007. [Google Scholar]
- Han J. From PID to active disturbance rejection control. Industrial Electronics IEEE transactions on, 2009, 56(3), pp.900–906. [CrossRef] [Google Scholar]
- Qi N M, Qin C M, Song Z G. Improved ADRC cascade decoupling controller design of hypersonic vehicle. Harbin Gongye Daxue Xuebao(Journal of Harbin Institute of Technology), 2011, 43(11), pp.34–38. [Google Scholar]
- Herbst G. A Simulative Study on Active Disturbance Rejection Control (ADRC) as a Control Tool for Practitioners. Electronics, 2013, 2(3), pp.246–279. [CrossRef] [Google Scholar]
- Ti. TMS320F28069M. TMS320F28068M InstaSPIN(TM) MOTION Software Technical Reference Manual: TEXAS INSTRUMENTS, 2013. [Google Scholar]
- Shaughnessy J D, Pinckney S Z, McMinn J D, Hypersonic vehicle simulation model: winged-cone configuration. NASA TM-102610, 1990. [Google Scholar]
- Huang Yi, Han Jing-qing.Analysis and design of nonlinear two-order continuous extended state observer.Chinese Science Bulletin, 2000, 45(13), pp. 1373–1379. [CrossRef] [Google Scholar]
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