Advanced Guidance and Control of Flight Vehicle: Theory and Application

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Bibliographic Details
Title: Advanced Guidance and Control of Flight Vehicle: Theory and Application
Contributors: Liang, Haizhao, Wang, Jianying, Liu, Chuang
Publisher Information: MDPI - Multidisciplinary Digital Publishing Institute
Publication Year: 2024
Collection: Directory of Open Access Books (DOAB)
Subject Terms: unmanned aerial vehicle, aircraft/engine integration, thrust optimization, adaptive margin model, adaptive disturbance rejection control, finite-time contractive stability, state feedback control, spacecraft rendezvous system, cone complementary linearization, C-W equations, particle swarm algorithm, UAV, 3D path planning, SHADE algorithm, three-dimensional engagement, maneuvering target, LOS angle rate, collision course, fixed-time convergence, trajectory tracking, uncertainty, extended kalman filter, adaptive, control constraints, T-MPSP, hypersonic entry, real-time trajectory planning, sequential convex programming, adaptive non-uniform discretization, feasibility guarantee
Description: The application of advanced guidance and control to missiles, hypersonic vehicles, and unmanned aerial vehicles has long represented a research hotspot in academia, and the development of more advanced and intelligent guidance and control technology for flight vehicles has become a focus of research in recent years. In this reprint, studies on the mathematical theory and application of flight vehicle guidance and control are presented. This includes trajectory optimization, online planning, advanced intermediate guidance theoretical methods, terminal guidance theoretical methods, intercept guidance and pursuit and escape guidance, and other topics.
Document Type: other/unknown material
File Description: application/octet-stream
Language: English
Relation: ONIX_20240906_9783725818853_28; https://mdpi.com/books/pdfview/book/9675
Availability: https://directory.doabooks.org/handle/20.500.12854/143666
https://hdl.handle.net/20.500.12854/143666
https://mdpi.com/books/pdfview/book/9675
Rights: open access
Accession Number: edsbas.8AF9F858
Database: BASE
Description
Abstract:The application of advanced guidance and control to missiles, hypersonic vehicles, and unmanned aerial vehicles has long represented a research hotspot in academia, and the development of more advanced and intelligent guidance and control technology for flight vehicles has become a focus of research in recent years. In this reprint, studies on the mathematical theory and application of flight vehicle guidance and control are presented. This includes trajectory optimization, online planning, advanced intermediate guidance theoretical methods, terminal guidance theoretical methods, intercept guidance and pursuit and escape guidance, and other topics.