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Mathematical Modelling and Control Theory for Aerospace Vehicles

A special issue of Mathematics (ISSN 2227-7390). This special issue belongs to the section "E2: Control Theory and Mechanics".

Deadline for manuscript submissions: 31 March 2026 | Viewed by 756

Special Issue Editor


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Guest Editor
School of Aerospace Engineering, Huazhong University of Science and Technology, 1037 Luoyu Road, Wuhan, China
Interests: aircraft guidance; control and trajectory optimization

Special Issue Information

Dear Colleagues,

We invite you to submit your latest applied research works in mathematical modelling and control theory for aerospace vehicles to this Special Issue, titled "Mathematical Modelling and Control Theory for Aerospace Vehicles".

Mathematical modelling provides effective theoretical support for aerodynamics, for the guidance and control of aerospace vehicles, and for the development of more advanced and intelligent mathematical modelling and control techniques for aerospace vehicles, which has become a significant research focus in recent years.

This Special Issue focuses on the mathematical modelling of complex dynamics problems, understanding flow control and complex flow phenomena, and the development and application of advanced and effective guidance and control methods. We welcome the submission of scientific articles on advanced and effective guidance and control methods that solve the problems associated with the following: trajectory optimization for aerospace vehicles, active flow control technology for high-speed vehicles, online planning and intelligent planning with high computational efficiency, advanced intermediate guidance theoretical methods, terminal guidance theoretical methods, intercept guidance and pursuit and escape guidance, nonlinear control, robust control, mathematical modelling of complex dynamics models, and so on. For this Special Issue, we encourage you to publish your most recent research works in the above fields and the results of simulation analyses and practical engineering.

Yours Sincerely,

Dr. Zhongtao Cheng
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 250 words) can be sent to the Editorial Office for assessment.

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. Mathematics is an international peer-reviewed open access semimonthly 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 2600 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

  • trajectory optimization
  • active flow control
  • online planning and intelligent planning
  • intermediate guidance
  • pursuit and escape guidance
  • nonlinear control and robust control
  • complex dynamics models

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Published Papers (1 paper)

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Research

21 pages, 2187 KB  
Article
Reliability-Adaptive Control of Aerospace Electromechanical Actuators with Coupled Degradation via Stochastic MPC
by Le Qi
Mathematics 2026, 14(4), 737; https://doi.org/10.3390/math14040737 - 22 Feb 2026
Viewed by 311
Abstract
Electromechanical Actuators (EMAs) are critical components in More-Electric Aircraft (MEA) and Reusable Launch Vehicles (RLVs), yet they remain vulnerable to jamming and fatigue failures under high-stress flight maneuvers. Existing Health-Aware Flight Control approaches often treat failure prediction and control allocation as separate processes, [...] Read more.
Electromechanical Actuators (EMAs) are critical components in More-Electric Aircraft (MEA) and Reusable Launch Vehicles (RLVs), yet they remain vulnerable to jamming and fatigue failures under high-stress flight maneuvers. Existing Health-Aware Flight Control approaches often treat failure prediction and control allocation as separate processes, leading to suboptimal sortie generation rates. This paper presents a reliability-adaptive control framework that unifies trajectory tracking with online health management. Empowered by a hierarchical mission-to-control architecture, the system employs stochastic Model Predictive Control (SMPC) to actively modulate control surface deflection profiles in real time. A comparative case study on a coupled EMA drivetrain demonstrates that the proposed controller extends useful life by 65% compared to fixed-gain baselines, achieves 23% higher mission performance than reactive PID controllers, and it maintains zero constraint violations throughout the mission by optimally distributing the health budget across mission phases. Full article
(This article belongs to the Special Issue Mathematical Modelling and Control Theory for Aerospace Vehicles)
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