Journal ArticleDOI
Finite-time convergent terminal guidance law design based on stochastic fast smooth second-order sliding mode
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TLDR
In this paper, a novel finite-time convergent terminal guidance law, based on stochastic fast smooth second-order sliding mode control theory, is proposed in order to handle the track imprecision caused mainly by inertial lag, model uncertainties and atmospheric environment disturbances, as well as the spatiotemporal noise caused by target maneuver term.About:
This article is published in Optik.The article was published on 2016-08-01. It has received 10 citations till now. The article focuses on the topics: Terminal guidance & Guidance system.read more
Citations
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Journal ArticleDOI
Review of advanced guidance and control algorithms for space/aerospace vehicles
Runqi Chai,Antonios Tsourdos,Al Savvaris,Senchun Chai,Yuanqing Xia,C. L. Philip Chen,C. L. Philip Chen +6 more
TL;DR: A systematic survey of state-of-the-art algorithms that are capable of generating reliable guidance and control commands for space/aerospace vehicles and particular focus is given to recent attempts to explore the possible uses of AI techniques in connection with the optimal control of the vehicle systems.
Journal ArticleDOI
Adaptive reaching law based three-dimensional finite-time guidance law against maneuvering targets with input saturation
YuJie Si,Shenmin Song +1 more
TL;DR: In this paper, the authors considered the problem of a missile intercepting a maneuvering target with impact angles constraints, and two finite-time guidance laws are proposed based on the coupled dynamics.
Book ChapterDOI
Performance Evaluation for the Sustainable Supply Chain Management
Xuemei Fan,Shujun Zhang +1 more
TL;DR: In this paper, the authors presented a model for SC performance evaluation using 5DBSC and Levenberg-Marquardt Back-propagation (LM•BP) neural network algorithm.
Journal ArticleDOI
Robust impact angle constraints guidance law with autopilot lag and acceleration saturation consideration
Junhong Song,Shenmin Song +1 more
TL;DR: A robust continuous guidance law with impact angle constraints in the presence of both an acceleration saturation constraint and a second-order-lag autopilot is developed for the three-dimensional terminal guidance problem of a missile intercepting a manoeuvring target.
Journal ArticleDOI
The three dimensional guidance system design of terminal attack phase for exo-atmospheric kill vehicle
TL;DR: The proposed guidance law is better attack precision than traditional guidance law, and the PWPF modulator with variable dead zone is more reasonable in fuel allocation and smaller on miss distance than traditional PWPf modulator.
References
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Proceedings ArticleDOI
On fixed and finite time stability in sliding mode control
TL;DR: Any finite-time convergent homogeneous sliding-mode controller can be transformed into a fixed- time convergent one, featuring an upper bound of convergence time, which does not depend on initial conditions.
BookDOI
Sliding Modes after the First Decade of the 21st Century
TL;DR: The book presents the newest results of the major world research groups working in the area of Variable Structure Systems and Sliding Mode Control (VSS/SMC).
Proceedings ArticleDOI
Integrated guidance and control of advanced interceptors using second order sliding modes
Y.B. Shtessel,I.A. Shkolnikov +1 more
TL;DR: In this article, a two-loop guidance and flight control system was designed in the combined state space of engagement kinematics and vehicle dynamics for the interceptor's trajectory prediction.
Related Papers (5)
An adaptive fast fixed-time guidance law with an impact angle constraint for intercepting maneuvering targets
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