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Wiley电子期刊(1)	SpringerLink电子期刊(72)	NATURE电子期刊(1)	Elsevier电子期刊(171)
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在“Elsevier电子期刊”中，命中：171条，耗时：0.0929552 秒

在所有数据库中总计命中：260条

1.An integrated guidance and control approach in three-dimensional space for hypersonic missile constrained by impact angles

作者：Xiaodong Liu ; ^{k.start@163.com} ; Wanwei Huang ^{wwhuang@163.com} ; Lifu Du ^{dulifu0328@163.com}

关键词：Dynamic surface control ; Dynamic inversion control ; Integrated guidance and control ; Nonlinear control ; Robust control

刊名：ISA Transactions

出版年：2017

2.A small-gain method for integrated guidance and control in terminal phase of reentry

作者：Han Yan ; ^{yhbice@gmail.com} ; Shuping Tan ; Yingzi He

关键词：Reusable launch vehicles ; Approach and landing phase ; Reference trajectory ; Integrated guidance and control ; Small-gain theorem ; Robustness

刊名：Acta Astronautica

出版年：2017

3.Physics-based simulation for manual robot guidance—An eRobotics approach

作者：Eric Guiffo Kaigom ; ^{kaigom@mmi.rwth-aachen.de" class="auth_mail" title="E-mail the corresponding author} ; ; Jü ; rgen Roß ; mann

关键词：Simulation-driven engineering ; Virtual testbeds ; Robot guidance

刊名：Robotics and Computer-Integrated Manufacturing

出版年：2017

4.Non-singular terminal dynamic surface control based integrated guidance and control design and simulation

作者：Zhang Cong^a ; ^b ; ^c ; Wu Yun-jie^a ; ^b ; ^c

关键词：Integrated guidance and control (IGC) ; Non-singular terminal sliding mode control (NTSMC) ; Dynamic surface control (DSC) ; Simulations

刊名：ISA Transactions

出版年：2016

5.Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure

作者：Weihong Wang^a ; ^b ; ^{wangww201507@163.com" class="auth_mail" title="E-mail the corresponding author} ; Shaofeng Xiong^a ; ^b ; ^c ; ^{shepinliu@163.com" class="auth_mail" title="E-mail the corresponding author} ; Sen Wang^a ; ^b ; ^{wangs201507@163.com" class="auth_mail" title="E-mail the corresponding author} ; Siyang Song^a ; ^b ; ^{songsy201507@163.com" class="auth_mail" title="E-mail the corresponding author} ; Chao Lai^a ; ^b ; ^{laic201507@163.com" class="auth_mail" title="E-mail the corresponding author}

关键词：Integrated guidance and control ; Input saturation ; Impact angle constraint ; Actuator failure ; Dynamic surface control ; Extended state observer

刊名：Aerospace Science and Technology

出版年：2016

6.Research on strap-down seeker guidance information for rolling interceptor

作者：Xiao Du ; ^{duxiao.63@163.com" class="auth_mail" title="E-mail the corresponding author} ; Qunli Xia

关键词：Strap-down seeker ; Rolling interceptor ; Decoupling method

刊名：Optik - International Journal for Light and Electron Optics

出版年：2017

7.Lateral guidance and control of UAVs using second-order sliding modes

作者：Syed Ussama Ali^a ; ^{ussama.ali@gmail.com" class="auth_mail" title="E-mail the corresponding author} ; Raza Samar^a ; ^{rsamar@jinnah.edu.pk" class="auth_mail" title="E-mail the corresponding author} ; M. Zamurad Shah^a ; ^{m.zamurad.2013@ieee.org" class="auth_mail" title="E-mail the corresponding author} ; Aamer I. Bhatti^a ; ^{aib@jinnah.edu.pk" class="auth_mail" title="E-mail the corresponding author} ; Khalid Munawar^b ; ^{munawar_khalid@yahoo.com" class="auth_mail" title="E-mail the corresponding author} ; Ubaid M. Al-Sggaf^b ; ^{usaggaf@kau.edu.sa" class="auth_mail" title="E-mail the corresponding author}

关键词：Sliding mode control ; Lateral guidance ; Higher order sliding mode ; Real twisting algorithm ; Super twisting algorithm ; Integrated guidance and control

刊名：Aerospace Science and Technology

出版年：2016

8.Robust partial integrated guidance and control for missiles via extended state observer

作者：Qing Wang^a ; Maopeng Ran^a ; ^{ranmp@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Chaoyang Dong^b

关键词：Partial integrated guidance and control ; Nonlinear systems ; Sliding mode control ; Extended state observer

刊名：ISA Transactions

出版年：2016

9.Integrated guidance and control for hypersonic vehicles in dive phase with multiple constraints

作者：JianHua Wang ; ^{WJH_NUDT_2013@163.com" class="auth_mail" title="E-mail the corresponding author} ; LuHua Liu ; Tun Zhao ; GuoJian Tang

关键词：Integrated guidance and control ; Dynamic surface control ; Adaptive control ; Impact angle constraints ; Hypersonic vehicle ; Dive phase

刊名：Aerospace Science and Technology

出版年：2016

10.Integrated guidance and control with L₂ disturbance attenuation for hypersonic vehicles

作者：Tun Zhao ; ^{zhaotun.aero@live.com" class="auth_mail" title="E-mail the corresponding author} ; Peng Wang ^{wonderful2020@163.com" class="auth_mail" title="E-mail the corresponding author} ; Luhua Liu ^{liu_luhua@sohu.com" class="auth_mail" title="E-mail the corresponding author} ; Jie Wu ^{wujie_nudt@sina.com" class="auth_mail" title="E-mail the corresponding author}

关键词：Integrated guidance and control ; Hypersonic vehicles ; L2 gain performance ; Backstepping design

刊名：Advances in Space Research

出版年：2016

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