Results 271 to 280 of about 5,368,406 (286)
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Journal of the Franklin Institute, 2020
In this paper, a new guidance law based on time-varying terminal sliding mode is proposed to make multi-agent intercept maneuvering target simultaneously. The new approach can make more benefits as follows: (1).
Sheng Zhai, Xiaoqian Wei, Jianying Yang
semanticscholar +1 more source
In this paper, a new guidance law based on time-varying terminal sliding mode is proposed to make multi-agent intercept maneuvering target simultaneously. The new approach can make more benefits as follows: (1).
Sheng Zhai, Xiaoqian Wei, Jianying Yang
semanticscholar +1 more source
Impact angle constraint guidance law using fully-actuated system approach
Aerospace Science and Technology, 2023Shi-wei Chen +3 more
semanticscholar +1 more source
Ocean Engineering, 2019
We present a novel nonlinear adaptive path following controller that compensates for drift forces though time-varying sideslip for amphibious hovercrafts.
Yuanhui Wang, Tong Haiyan, Mingyu Fu
semanticscholar +1 more source
We present a novel nonlinear adaptive path following controller that compensates for drift forces though time-varying sideslip for amphibious hovercrafts.
Yuanhui Wang, Tong Haiyan, Mingyu Fu
semanticscholar +1 more source
Sliding Mode Guidance Law for Impact Time Control Without Explicit Time-to-Go Estimation
IEEE Transactions on Aerospace and Electronic Systems, 2019This paper presents an impact time control guidance law that does not perform explicit time-to-go estimation. In order to satisfy the interception and the desired impact time constraint simultaneously, a sliding surface variable formulated as a sum of ...
Hyeong-Geun Kim, Dongsoo Cho, H. J. Kim
semanticscholar +1 more source
Backstepping-Based Impact Time Control Guidance Law for Missiles With Reduced Seeker Field-of-View
IEEE Transactions on Aerospace and Electronic Systems, 2019This paper proposes a guidance law that achieves the desired terminal impact time without violating a seeker's field-of-view (FOV) limits. In order to derive the guidance law, kinematic conditions for impact time control are defined, and the backstepping
Hyeong-Geun Kim +2 more
semanticscholar +1 more source
Fractional-order sliding mode control based guidance law with impact angle constraint
Nonlinear dynamics, 2021Y. Sheng, Zhuo Zhang, Lei Xia
semanticscholar +1 more source
International Journal of Control, Automation and Systems, 2022
Chao Ming, Xiaoming Wang
semanticscholar +1 more source
Chao Ming, Xiaoming Wang
semanticscholar +1 more source
Three-dimensional cooperative guidance law for intercepting hypersonic targets
Aerospace Science and Technology, 2022Shuangxi Liu +5 more
semanticscholar +1 more source

