Intelligent Design, Control and Perception for Unmanned Aerial System

A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".

Deadline for manuscript submissions: closed (31 July 2023) | Viewed by 2914

Special Issue Editors


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Guest Editor
Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China
Interests: overall design of unmanned systems; flight dynamics and control of UAV; multi-domain unmanned system design
Special Issues, Collections and Topics in MDPI journals
State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong University, Xi’an 710049, China
Interests: flight vehicle design; aerodynamic optimization; flow control; turbulence modeling and UAV design

Special Issue Information

Dear Colleagues,

Unmanned aerial systems (UAS) have had a significant influence in the modern period. Due to UAS’s high efficiency and low cost, a great deal of study has been conducted on these subjects. Numerous conveniences, including as parcel transportation, reconnaissance of uncharted regions, and relay communication, have been made possible by UAS. The rapid growth of UAS has resulted in a multitude of unique applications that have, are, and will alter a great number of civil and military aviation traditions. However, the prospective applications of UAS cannot be limited by the current state of research. The most up-to-date approaches and technology are certain to spark fresh ideas or possibly a revolution in UAS’s design and implementation. 

The disciplines connected to design, control, and perception across the academic and industrial spectrum frequently provide new understandings and experiences from the most prevalent use of UAS. In addition, the development of intelligent technology has increased not only the efficacy but also the accuracy of the aforementioned three factors. The most recent advancements in configuration, aerodynamic performance, and structural strength of UAS have provided very compelling evidence that many insights from natural beings can be applied at a very low cost and without causing injury or death, thereby making it possible to relax the rules that must be observed by manned vehicles. Numerous control algorithms may now be tested and implemented in ways that were impossible even a few years ago, allowing them to complete numerous missions that cannot be handled by humans. As sensors become smaller and more precise, UAVs can be outfitted as perceptual units to collect data from inaccessible places and assist or perhaps replace humans in decision-making. Consequently, how UAVs should be used to perceive new environmental data is a very intriguing issue that must be thoroughly investigated to determine its advantages and cons.

Above, we solicit articles that either address the research opportunities described here or that make a substantial addition to the state of the art in the broader field of UAS.

Dr. Min Chang
Dr. Yang Zhang
Guest Editors

Manuscript Submission Information

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Keywords

  • unmanned aerial system
  • intelligent perception and positioning
  • aerodynamic simulation
  • optimization in aerodynamics or structures
  • multi-UAVs control
  • unmanned systems effectiveness evaluation
  • aircraft design and optimization
  • aerospace propulsion
  • smart materials and aircraft structures design
  • rotorcraft
  • flight dynamics

Published Papers (2 papers)

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Research

27 pages, 7410 KiB  
Article
A Low-Cost Relative Positioning Method for UAV/UGV Coordinated Heterogeneous System Based on Visual-Lidar Fusion
by Haojun Luo and Chih-Yung Wen
Aerospace 2023, 10(11), 924; https://doi.org/10.3390/aerospace10110924 - 29 Oct 2023
Viewed by 1358
Abstract
Unmanned Ground Vehicles (UGVs) and Unmanned Aerial Vehicles (UAVs) are commonly used for various purposes, and their cooperative systems have been developed to enhance their capabilities. However, tracking and interacting with dynamic UAVs poses several challenges, including limitations of traditional radar and visual [...] Read more.
Unmanned Ground Vehicles (UGVs) and Unmanned Aerial Vehicles (UAVs) are commonly used for various purposes, and their cooperative systems have been developed to enhance their capabilities. However, tracking and interacting with dynamic UAVs poses several challenges, including limitations of traditional radar and visual systems, and the need for the real-time monitoring of UAV positions. To address these challenges, a low-cost method that uses LiDAR (Light Detection and Ranging) and RGB-D cameras to detect and track UAVs in real time has been proposed. This method relies on a learning model and a linear Kalman filter, and has demonstrated satisfactory estimation accuracy using only CPU (Central Processing Unit)- in GPS (Global Positioning System)-denied environments without any prior information. Full article
(This article belongs to the Special Issue Intelligent Design, Control and Perception for Unmanned Aerial System)
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14 pages, 4324 KiB  
Article
Receptivity and Stability Theory Analysis of a Transonic Swept Wing Experiment
by Yuanqiang Liu, Yan Liu, Zubi Ji, Yutian Wang and Jiakuan Xu
Aerospace 2023, 10(10), 903; https://doi.org/10.3390/aerospace10100903 - 23 Oct 2023
Viewed by 1044
Abstract
Surface suction provides an efficient way to delay boundary layer transitions. In order to verify the suction effects and determine the mechanism of suction control in transonic swept wing boundary layers, wind tunnel transition measurements in a hybrid laminar flow control (HLFC) wind [...] Read more.
Surface suction provides an efficient way to delay boundary layer transitions. In order to verify the suction effects and determine the mechanism of suction control in transonic swept wing boundary layers, wind tunnel transition measurements in a hybrid laminar flow control (HLFC) wind tunnel model uses an infrared thermography technique in the Aircraft Research Association (ARA) 2.74 m × 2.44 m low turbulence level transonic wind tunnel. Based on the experimental data of stationary crossflow dominant transitions without and with surface suction in transonic swept wing boundary layers, in this paper, the effects on the receptivity and linear and nonlinear evolution of stationary crossflow vortices have been analyzed with the consideration of curvature. Theoretical analysis agreed with the experimental observations in regard to the transition delay caused by boundary layer suction near the leading-edge region. Full article
(This article belongs to the Special Issue Intelligent Design, Control and Perception for Unmanned Aerial System)
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