Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review

S Liu, B Yan, W Huang, X Zhang, J Yan - Journal of Zhejiang University …, 2023 - Springer
The unique performance advantages of hypersonic vehicles represent a critical challenge
for existing defense systems. To facilitate defensive operations against hypersonic vehicles …

[图书][B] Robust control of supercavitating vehicles in the presence of dynamic and uncertain cavity

A Goel - 2005 - search.proquest.com
Underwater travel is greatly limited by the speed that can be attained by the vehicles.
Usually, the maximum speed achieved by underwater vehicles is about 40 m/s …

Tuning of a linear-quadratic stabilization system for an anti-aircraft missile

W Bużantowicz - Aerospace, 2021 - mdpi.com
A description is given of an application of a linear-quadratic regulator (LQR) for stabilizing
the characteristics of an anti-aircraft missile, and an analytical method of selecting the …

Application of fuzzy logic in engineering problems

A Gad, M Farooq - IECON'01. 27th Annual Conference of the …, 2001 - ieeexplore.ieee.org
In today's fast paced world of increasing and innovative new technology, fuzzy logic is a
practical mathematical addition to classic Boolean logic. We can see its applications in many …

Design of an adaptive gust response alleviation control system: simulations and experiments

K Shao, Z Wu, C Yang, L Chen, B Lv - Journal of Aircraft, 2010 - arc.aiaa.org
GUSTS can adversely affect large aircraft during high-speed cruising and turns. They not
only cause the aircraft to produce an unexpected additional overload, but they also easily …

Self-organizing fuzzy learning CLOS guidance law design

CM Lin, CF Hsu, YJ Mon - IEEE Transactions on Aerospace …, 2003 - ieeexplore.ieee.org
A new self-organizing fuzzy logic control (SOFLC) design method is proposed. The
proposed method is applied to the command line-of-sight (CLOS) guidance law design. The …

Predictive guidance of a projectile for hit-to-kill interception

PV Hahn, RA Frederick… - IEEE Transactions on …, 2009 - ieeexplore.ieee.org
In this paper, a predictive guidance algorithm is developed for a spin-stabilized hit-to-kill
guided projectile. The projectile is used as an interceptor against rockets, mortar, and …

基于模糊变系数策略的迎击拦截变结构制导律设计

熊俊辉, 唐胜景, 郭杰, 朱大林 - 兵工学报, 2014 - co-journal.com
迎击拦截是拦截问题中常见的一种制导方式. 为提高拦截器的末制导精度,
基于变结构控制设计零化视线角速率的变结构制导律是一种典型方法. 对高速目标的迎击拦截 …

An observer-based continuous adaptive sliding mode guidance against chattering for homing missiles

J Guo, Y Li, J Zhou - … of the Institute of Measurement and …, 2019 - journals.sagepub.com
A novel observer-based continuous adaptive sliding mode guidance (OCASMG) is
proposed for homing missiles. First, a new sliding mode guidance law is derived from the …

Nonlinear rule-based controller for missile terminal guidance

CS Shieh - IEE Proceedings-Control Theory and Applications, 2003 - IET
The design of a rule-based guidance law for homing missiles onto targets is presented. The
stability of the missile-target dynamics is proven. Unlike conventional approaches that solve …