Dynamic Control for High-Speed Flights
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: 30 April 2026 | Viewed by 51
Special Issue Editor
Interests: guidance and control; optimal control; trajectory planning; learning (artificial intelligence)
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
We sincerely invite you to submit your latest applied research in the field of the application of guidance and control to missiles, hypersonic vehicles, and unmanned aerial vehicles to this Special Issue entitled "Dynamic Control for High-Speed Flights". The dynamics and control technology for high-speed flights has always been a research hotspot in academia. Specifically, how to provide more advanced and intelligent dynamics modeling and control technology for high-speed flight vehicles has become a research focus in recent years. This kind of problem involves many mathematical theories and applications. Therefore, the purpose of this Special Issue is to conduct in-depth research on the mathematical theory and application of high-speed flight vehicle dynamics and control. For this Special Issue, we welcome the submissions of scientific articles on the following topics: advanced and effective dynamics modeling and control methods for solving problems of complex dynamics models; trajectory optimization of flight vehicles; online and intelligent planning with high computational efficiency; advanced intermediate guidance theoretical methods; terminal guidance theoretical methods; intercept guidance; pursuit and escape guidance; nonlinear control; robust control; simulation analysis results; practical engineering applications; etc.
We look forward to receiving your contributions.
Dr. Jianying Wang
Guest Editor
Manuscript Submission Information
Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.
Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Aerospace is an international peer-reviewed open access monthly journal published by MDPI.
Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2400 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.
Keywords
- missiles
- hypersonic vehicles
- unmanned aerial vehicles
- high-speed vehicle models
- trajectory optimization
- tracking guidance
- terminal guidance
- intelligent guidance
- attitude control
- nonlinear control
- robust control
- intelligent control
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