Dynamics and Control of Aerospace Systems—2nd Edition

A special issue of Actuators (ISSN 2076-0825). This special issue belongs to the section "Aerospace Actuators".

Deadline for manuscript submissions: 30 June 2025 | Viewed by 947

Special Issue Editors


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Guest Editor
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Interests: dynamics modelling; cooperative control; drone systems; attitude control; on-orbit assembly; vibration control
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Guest Editor
Laboratory of Hydrodynamics, Energy and Atmospheric Environment, Ecole Centrale de Nantes, CEDEX 3, 44321 Nantes, France
Interests: dynamics and control of tethered spacecraft system; model predictive control strategy; state identification and estimation; novel concept of space structure; solid mechanics and finite element method
Special Issues, Collections and Topics in MDPI journals

E-Mail
Guest Editor
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Interests: dynamics and control of spacecraft cluster

E-Mail Website
Guest Editor
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Interests: dynamics and control of space tether systems; nonlinear vibration control

Special Issue Information

Dear Colleagues,

The dynamics and control of aerospace systems have attracted growing interest due to them being key problems in the development of aerospace vehicles such as space stations, space telescopes, and advanced aircraft. The purpose of dynamics is to study system behaviours using time and force, while the purpose of control is to develop the control effect with error feedback under various working conditions. Knowledge of aerospace systems is critical for the design of control systems. Newly designed aerospace systems raise novel challenges for dynamics and control techniques. We invite investigators to contribute original research and review articles addressing dynamics modelling, stability analysis, and controller design of aerospace systems.

Potential topics include, but are not limited to, the following:

  • Control system design of aircraft and spacecraft;
  • System modelling, analysis, and identification of aerospace systems;
  • System stability of aerospace vehicles;
  • Sensors and control actuators of aircraft, rockets, and spacecraft;
  • Orbit and attitude dynamics and control;
  • Drone dynamics and control;
  • Space tether dynamics and control;
  • Experimental investigation of aerospace systems;
  • Novel sensors and actuators of aerospace vehicles.

Prof. Dr. Ti Chen
Dr. Gangqiang Li
Dr. Zhengtao Wei
Dr. Caoqun Luo
Guest Editors

Manuscript Submission Information

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Keywords

  • system dynamics
  • system identification
  • control system design
  • stability analysis
  • dynamics and control
  • aerospace vehicles
  • experimental investigation

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Published Papers (1 paper)

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Research

16 pages, 6005 KiB  
Article
Nonlinear Optimal Control for Spacecraft Rendezvous and Docking Using Symplectic Numerical Method
by Zhengtao Wei, Jie Yang, Hao Wen, Dongping Jin and Ti Chen
Actuators 2025, 14(2), 75; https://doi.org/10.3390/act14020075 - 6 Feb 2025
Cited by 1 | Viewed by 654
Abstract
This paper addresses the autonomous rendezvous and docking between a chaser spacecraft and a target spacecraft. An optimal control method is employed to plan the rendezvous and docking maneuver, considering various constraints, including force, velocity, field of view, and collision avoidance with a [...] Read more.
This paper addresses the autonomous rendezvous and docking between a chaser spacecraft and a target spacecraft. An optimal control method is employed to plan the rendezvous and docking maneuver, considering various constraints, including force, velocity, field of view, and collision avoidance with a diamond-shaped obstacle. The optimal trajectories are derived using a symplectic algorithm, which ensures high accuracy and enhances computational efficiency. These trajectories serve as the reference for the maneuver. A PD-based tracking control method is proposed to enable real-time feedback control. An air-bearing experimental system, encompassing state measurement, data transmission, and processing, is established to conduct ground-based tracking experiments. Furthermore, specialized simulators for the chaser and target spacecraft, equipped with a docking mechanism, are designed. Experimental results validate both the feasibility of the reference trajectories and the effectiveness of the PD tracking control approach. Full article
(This article belongs to the Special Issue Dynamics and Control of Aerospace Systems—2nd Edition)
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