Skip to Content

Aerospace, Volume 12, Issue 7

2025 July - 84 articles

Cover Story: Accurate aerodynamic models are vital for missile control. This paper, using wind tunnel data, analyzes how modeling errors influence missile dynamics and control. We compare methods and test longitudinal coefficient deviations. The key findings are as follows: interpolation risks overfitting; denser Mach testing or segmentation improves accuracy; and derivative/coefficient error models enable faster uncertainty studies within limited envelopes. Crucially, only CLα, CmCL, and Cmq affect longitudinal eigenvalues. The lift/pitch control frequency difference dictates non-minimum phase behavior. Critically, aerodynamic uncertainties amplify overshoot risk, necessitating robust control design to counter modeling imperfections. View this paper
  • Issues are regarded as officially published after their release is announced to the table of contents alert mailing list .
  • You may sign up for email alerts to receive table of contents of newly released issues.
  • PDF is the official format for papers published in both, html and pdf forms. To view the papers in pdf format, click on the "PDF Full-text" link, and use the free Adobe Reader to open them.

Articles (84)

  • Article
  • Open Access
2 Citations
3,064 Views
26 Pages

Experimental Acoustic Investigation of Rotor Noise Directivity and Decay in Multiple Configurations

  • Giovanni Fasulo,
  • Giosuè Longobardo,
  • Fabrizio De Gregorio and
  • Mattia Barbarino

In the framework of the MATIM project, an acoustic test campaign was conducted on a platform derived from a commercial-class quadcopter within the CIRA semi-anechoic chamber. A dedicated rotor rig allowed systematic measurements of thrust, torque, an...

(This article belongs to the Special Issue New Developments in Aeroacoustics Research: From Fundamentals to Applications)
  • Article
  • Open Access
1 Citations
1,075 Views
16 Pages

During the process of flexible aerial refueling, the flexible structure of the hose drogue assembly is affected by internal and external interference, such as docking maneuvering, deformation of the hose, attitude changes, and body vibrations, causin...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
7 Citations
3,215 Views
32 Pages

A Comparative Study of Unsupervised Deep Learning Methods for Anomaly Detection in Flight Data

  • Sameer Kumar Jasra,
  • Gianluca Valentino,
  • Alan Muscat and
  • Robert Camilleri

This paper provides a comparative study of unsupervised Deep Learning (DL) methods for anomaly detection in Flight Data Monitoring (FDM). The paper applies Long Short-Term Memory (LSTM), Gated Recurrent Units (GRUs), Convolutional Neural Network (CNN...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
3 Citations
2,671 Views
23 Pages

The aerodynamic optimization of airfoil shapes remains a critical research area for enhancing aircraft performance under various flight conditions. In this study, the RAE 2822 airfoil was selected as a benchmark case to investigate and compare the ef...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,435 Views
32 Pages

In airport operations management, accurately estimating the service durations of ground support equipment such as Potable Water Trucks (PWTs) is essential for improving resource allocation efficiency and ensuring timely aircraft turnaround. Tradition...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
2 Citations
2,157 Views
25 Pages

Visual Active SLAM Method Considering Measurement and State Uncertainty for Space Exploration

  • Yao Zhao,
  • Zhi Xiong,
  • Jingqi Wang,
  • Lin Zhang and
  • Pascual Campoy

This paper presents a visual active SLAM method considering measurement and state uncertainty for space exploration in urban search and rescue environments. An uncertainty evaluation method based on the Fisher Information Matrix (FIM) is studied from...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
3,005 Views
30 Pages

A DSP–FPGA Heterogeneous Accelerator for On-Board Pose Estimation of Non-Cooperative Targets

  • Qiuyu Song,
  • Kai Liu,
  • Shangrong Li,
  • Mengyuan Wang and
  • Junyi Wang

The increasing presence of non-cooperative targets poses significant challenges to the space environment and threatens the sustainability of aerospace operations. Accurate on-orbit perception of such targets, particularly those without cooperative ma...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
2 Citations
1,224 Views
17 Pages

A turboprop aircraft is exposed to the risk of bird strikes during flight, which may have a serious impact on flight safety once the bird is sucked into the engine. In this study, the aerodynamic and bird exclusion characteristics of a branched turbo...

(This article belongs to the Special Issue Environmental Influences on Aircraft Aerodynamics)
  • Article
  • Open Access
1 Citations
1,216 Views
36 Pages

The terminal maneuvering area (TMA) serves as a critical transition zone between upper enroute airways and airports, representing one of the most complex regions for managing high volumes of arrival and departure traffic. This paper presents the mult...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
6 Citations
1,079 Views
25 Pages

The velocity distribution at the deflector jet outlet significantly influences the pressure characteristics of the pilot stage, thereby affecting the dynamic performance of the servo valve. Conventional mathematical models fail to account for the inf...

(This article belongs to the Special Issue Aerospace Vehicles and Complex Fluid Flow Modelling)
  • Article
  • Open Access
2 Citations
1,202 Views
20 Pages

A Novel Shape Memory Alloy Actuated Bearing Active Preload System (SMA-BAPS) for Space Spindles

  • Yuhang Zhang,
  • Jun Jiang,
  • Qiang Zhang,
  • Yuanzi Zhou,
  • Xiaoyong Zhang and
  • Ruijie Sun

In this study, a novel shape memory alloy actuated bearing active preload system (SMA-BAPS) was proposed and experimentally demonstrated. SMA actuators placed in a single or antagonistic configuration were employed to drive the screw pair and thus fu...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1,625 Views
16 Pages

Aircraft wing surface icing compromises flight safety, where accurate calculation of heat transfer coefficient on airfoil surfaces serves as a prerequisite for designing thermal anti-icing systems. However, during icing conditions, ice morphology cha...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,538 Views
15 Pages

The Engine Electronic Controller (EEC), as the core component of an aircraft engine control system, is vulnerable to rapid failure when exposed to thermal shock during engine fire incidents, potentially leading to catastrophic aviation accidents. To...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
1,695 Views
32 Pages

The ability to collaborate with new teammates, adapt to unfamiliar environments, and engage in effective planning is essential for multi-drone agents within unmanned combat systems. This paper introduces DETEAMSK (Model-based Reinforcement Learning b...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
4 Citations
2,225 Views
17 Pages

On-Orbit Life Prediction and Analysis of Triple-Junction Gallium Arsenide Solar Arrays for MEO Satellites

  • Huan Liu,
  • Chenjie Kong,
  • Yuan Shen,
  • Baojun Lin,
  • Xueliang Wang and
  • Qiang Zhang

This paper focuses on the triple-junction gallium arsenide solar array of a MEO (Medium Earth Orbit) satellite that has been in orbit for 7 years. Through a combination of theoretical and data-driven methods, it conducts research on anti-radiation de...

  • Article
  • Open Access
1 Citations
1,254 Views
27 Pages

For the airfoil in freestream, the pressure difference between the upper and lower surfaces and the variations in pressure gradients are significant at its leading edge area. Under reasonable deflections, the active leading edge can effectively chang...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
2,385 Views
15 Pages

By assuming that both travel and departure time are normally distributed variables, a multi-objective stochastic optimization model for the multi-airport flight cooperative scheduling problem (MAFCSP) with CvaR of travel and departure time is firstly...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
2 Citations
1,503 Views
23 Pages

Predicting Electromagnetic Performance Under Wrinkling in Thin-Film Phased Arrays

  • Xiaotao Zhou,
  • Jianfei Yang,
  • Lei Zhang,
  • Huanxiao Li,
  • Xin Jin,
  • Yesen Fan,
  • Yan Xu and
  • Xiaofei Ma

Deployable thin-film antennas deliver large aperture gains and high stowage efficiency for spaceborne phased arrays but suffer wrinkling-induced planarity loss and radiation distortion. To bridge the lack of electromechanical coupling models for tens...

(This article belongs to the Special Issue Space Mechanisms and Robots)
  • Article
  • Open Access
2 Citations
1,993 Views
22 Pages

Visual Detection on Aircraft Wing Icing Process Using a Lightweight Deep Learning Model

  • Yang Yan,
  • Chao Tang,
  • Jirong Huang,
  • Zhixiong Cen and
  • Zonghong Xie

Aircraft wing icing significantly threatens aviation safety, causing substantial losses to the aviation industry each year. High transparency and blurred edges of icing areas in wing images pose challenges to wing icing detection by machine vision. T...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
994 Views
16 Pages

With the advancement of the third-generation BeiDou Navigation Satellite System (BDS-3), BeiDou dual-frequency multi-constellation (DFMC) receivers exhibit distinct advantages in accuracy and reliability due to their dual-frequency capabilities. Howe...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
1,631 Views
21 Pages

A cooperative game negotiation strategy considering multiple constraints is proposed for distributed impulsive multi-spacecraft approach missions in the presence of defending spacecraft. It is a dual-stage decision-making method that includes offline...

(This article belongs to the Section Astronautics & Space Science)
  • Review
  • Open Access
11 Citations
8,482 Views
21 Pages

Flight deck automation changes the nature of traditional piloting tasks, ultimately changing the cognitive requirements of the pilot. It is unclear how pilot performance should be measured as automation increases. The objective of this work is to und...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
1 Citations
2,093 Views
15 Pages

The research and development of the next generation of supersonic transports (SSTs) meets economic and environmental problems. An SST encounters critical challenges, including the need for low fuel consumption, low noise, and low gas emissions. Curre...

(This article belongs to the Special Issue Research and Development of Supersonic Aircraft)
  • Article
  • Open Access
1 Citations
1,845 Views
19 Pages

Analysis of Liquid Xenon Tank Filling Process in Different Gravity Environments

  • Zong-Yu Wu,
  • Chao Jiang,
  • Yong Chen,
  • Kai Li,
  • Yiyong Huang and
  • Yun Cheng

With the advancement in deep-space exploration, the injection technology using xenon as a working fluid in electric propulsion systems has emerged as a key area of interest. To delve into the gas-liquid dynamics of the liquid xenon injection process...

(This article belongs to the Special Issue Numerical Simulations in Electric Propulsion)
  • Article
  • Open Access
1,538 Views
16 Pages

Analysis of Vibration Characteristics of Angular Contact Ball Bearings in Aviation Engines Under Changing Conditions

  • Yanfang Dong,
  • Zibo Yan,
  • Jianyong Sun,
  • Wei Yu,
  • Hai Zhang,
  • Wenbo Zhou and
  • Jihao Jin

This paper addresses the vibration characteristics of angular contact ball bearings in aircraft engines under variable load conditions. Based on multibody dynamics theory, a dynamic model of the bearing was established. Vibration data under actual op...

  • Article
  • Open Access
2 Citations
1,424 Views
10 Pages

Prediction of Propellant Electrostatic Sensitivity Based on Small-Sample Machine Learning Models

  • Fei Wang,
  • Kai Cui,
  • Jinxiang Liu,
  • Wenhai He,
  • Qiuyu Zhang,
  • Weihai Zhang and
  • Tianshuai Wang

Hydroxyl-terminated-polybutadiene (HTPB)-based composite solid propellants are extensively used in aerospace and defense applications due to their high energy density, thermal stability, and processability. However, the presence of highly sensitive e...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
3 Citations
2,209 Views
27 Pages

Investigation of Improved Labyrinth Seal Stability Accounting for Radial Deformation

  • Guozhe Ren,
  • Hongyuan Tang,
  • Dan Sun,
  • Wenfeng Xu and
  • Yu Li

This study examines the labyrinth seal disc of an aero-engine, specifically analysing the radial deformation caused by centrifugal force and heat stress during operation. This distortion may lead to discrepancies in the performance attributes of the...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
4,619 Views
19 Pages

The Lunar Augmented Navigation Service (LANS) is the lunar equivalent of GNSS for future lunar explorations. It offers users accurate position, navigation, and timing (PNT) capabilities on and around the Moon. The Augmented Forward Signal (AFS) is a...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
2,158 Views
18 Pages

Flight mechanics/dynamics models are essential for analyzing aircraft flight performance, where aerodynamic data play a critical role. This paper establishes a missile flight dynamics model and investigates the influence of aerodynamic modeling error...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
3 Citations
1,521 Views
25 Pages

Optimal Midcourse Guidance with Terminal Relaxation and Range Convex Optimization

  • Jiong Li,
  • Jinlin Zhang,
  • Jikun Ye,
  • Lei Shao and
  • Xiangwei Bu

In midcourse guidance, strong constraints and dual-channel control coupling pose major challenges for trajectory optimization. To address this, this paper proposes an optimal guidance method based on terminal relaxation and range convex programming....

(This article belongs to the Special Issue Dynamics, Guidance and Control of Aerospace Vehicles)
  • Article
  • Open Access
2 Citations
3,529 Views
17 Pages

Development of a Throttleable 6 kN H2O2/Butyl Alcohol Rocket Engine

  • Zbigniew Gut,
  • Adrian Parzybut and
  • David Perigo

The increasing demand for versatile and sustainable propulsion systems has intensified research into green propellants and advanced thrust modulation technologies. This study presents the development and testing of a throttleable rocket engine utiliz...

(This article belongs to the Special Issue Green Propellants for In-Space Propulsion)
  • Article
  • Open Access
2 Citations
1,102 Views
31 Pages

Resolving Non-Proportional Frequency Components in Rotating Machinery Signals Using Local Entropy Selection Scaling–Reassigning Chirplet Transform

  • Dapeng Quan,
  • Yuli Niu,
  • Zeming Zhao,
  • Caiting He,
  • Xiaoze Yang,
  • Mingyang Li,
  • Tianyang Wang,
  • Lili Zhang,
  • Limei Ma and
  • Hongtao Wu
  • + 1 author

Under complex operating conditions, vibration signals from rotating machinery often exhibit non-stationary characteristics with non-proportional and closely spaced instantaneous frequency (IF) components. Traditional time–frequency analysis (TF...

  • Article
  • Open Access
4 Citations
1,613 Views
20 Pages

With the in-depth study of the unique flight ability of bats in the field of bionic robots, wind-tunnel experiments have become an important means to verify the feasibility of bat-like flying robot structures. However, due to the complex structure of...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
1,275 Views
22 Pages

The assembly optimization design of satellite components is a crucial element in the overall design of satellites. In this paper, a novel three-dimensional assembly optimization design problem (3D-AODP) for multi-module micro–nano satellite com...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
2 Citations
1,880 Views
19 Pages

A Stackelberg equilibrium–based Model Reference Adaptive Control (MSE) method is proposed for spacecraft Pursuit–Evasion (PE) games with incomplete information and sequential decision making under a non–zero–sum framework. Fir...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
9 Citations
1,786 Views
13 Pages

STHFD: Spatial–Temporal Hypergraph-Based Model for Aero-Engine Bearing Fault Diagnosis

  • Panfeng Bao,
  • Wenjun Yi,
  • Yue Zhu,
  • Yufeng Shen and
  • Boon Xian Chai

Accurate fault diagnosis in aerospace transmission systems is essential for ensuring equipment reliability and operational safety, especially for aero-engine bearings. However, current approaches relying on Convolutional Neural Networks (CNNs) for Eu...

(This article belongs to the Special Issue Challenges and Recent Advances in Model-Based Engineering for Aerospace)
  • Article
  • Open Access
4 Citations
2,692 Views
27 Pages

This paper investigates flexible multibody dynamic modeling and a staged deployment strategy for large-scale spinning tethered satellite systems, targeting deployment instability, inefficiencies, and tension-induced fracture risks. A nonlinear flexib...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
2 Citations
1,756 Views
23 Pages

This article proposes a method to solve nonlinear optimal control problems with arbitrary performance indices and terminal constraints, which is based on the neighboring extremal method and Gauss pseudospectral collocation. Firstly, a quadratic perfo...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
3 Citations
5,632 Views
13 Pages

Since 1957, the near-Earth population of trackable space objects has grown in number to over 36,000. Of these 36,000+ trackable objects now in low Earth orbit, just a few thousand are working spacecraft. The rest are Earth-orbiting objects which are...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
3 Citations
968 Views
22 Pages

Effect of Slide Valve Gap Surface Roughness on Particle Transport Properties

  • Jin Zhang,
  • Ranheng Du,
  • Pengpeng Dong,
  • Kuohang Zhang,
  • Shengrong Wang,
  • Ying Li and
  • Kuo Zhang

Fuel electro-hydraulic servo valves are core components in the fuel control system of aero-engines, and their performance directly affects thrust regulation and power output precision. Due to the combustibility of the working medium in fuel systems a...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
1,938 Views
28 Pages

This study proposes a novel paradigm for enhancing the fault detection and isolation (FDI) of gas generators in all-electric auxiliary power unit (APU) by utilizing shaft power information from the starter/generator. First, we conduct an investigatio...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
2,638 Views
19 Pages

With the increased proliferation of drone use for many purposes, counter drone technology has become crucial. This rapid expansion has inherently introduced significant opportunities and applications. This creates applications such as aerial surveill...

(This article belongs to the Special Issue Advances in UAV Technology: Dynamics, Guidance, Navigation, and Control of Transformative Aerial Vehicles)
  • Article
  • Open Access
1 Citations
2,161 Views
23 Pages

The goal of this paper is to optimize mission schedules for vertical airports (vertiports in short) to satisfy the different needs of stakeholders. We model the problem as a resource-constrained project scheduling problem (RCPSP) to obtain the best r...

(This article belongs to the Special Issue Next-Generation Airport Operations and Management)
  • Review
  • Open Access
2 Citations
4,239 Views
28 Pages

A Review on Liquid Pulsed Laser Propulsion

  • Sai Li,
  • Baosheng Du,
  • Qianqian Cui,
  • Jifei Ye,
  • Haichao Cui,
  • Heyan Gao,
  • Ying Wang,
  • Yongzan Zheng and
  • Jianhui Han

Laser propulsion is a new conceptual technology that drives spacecraft and possesses advantages such as high specific impulse, large payload ratio, and low launch cost. It has potential applications in diverse areas, such as space debris mitigation a...

(This article belongs to the Special Issue Laser Propulsion Science and Technology (2nd Edition))
  • Article
  • Open Access
2,314 Views
15 Pages

Common-mode analysis (CMA) is a qualitative analytical method used to support the evaluation of independence in the system safety assessment of civil aircraft. In traditional CMA, independence requirements are usually identified by evaluating the com...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
5 Citations
3,484 Views
37 Pages

Braking systems are essential to aircraft safety and operational efficiency; however, the variability of carbon brake wear, driven by the intricate interplay of operational and environmental factors, presents challenges for effective maintenance plan...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
2 Citations
2,884 Views
34 Pages

A collaborative inter-laboratory study was conducted to characterise the performance of the novel 250 W External Discharge Plasma Thruster (XPT) with a channel-less Hall effect-type thruster designed to address lifetime limitations and lower-power ef...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
3,702 Views
24 Pages

This study presents the development of a manufacturing process for a double-serpentine (DS) exhaust nozzle for unmanned aerial vehicles (UAVs) based on carbon fiber-reinforced silicon carbide matrix composites (C/SiCs). The DS nozzle is designed to r...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
4 Citations
1,733 Views
26 Pages

An aircraft that has been carefully optimized for a single flight condition will tend to perform poorly at other flight conditions. For aircraft such as long-haul airliners, this is not necessarily a problem, since the cruise condition so heavily dom...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
2,367 Views
30 Pages

Design to Deployment: Flight Schedule-Based Analysis of Hybrid Electric Aircraft Variants in U.S. Regional Carrier Operations

  • Emma Cassidy,
  • Paul R. Mokotoff,
  • Yilin Deng,
  • Michael Ikeda,
  • Kathryn Kirsch,
  • Max Z. Li and
  • Gokcin Cinar

This study evaluates the feasibility and benefits of introducing battery-powered hybrid electric aircraft (HEA) into regional airline operations. Using 2019 U.S. domestic flight data, the ERJ175LR is selected as a representative aircraft, and several...

(This article belongs to the Section Aeronautics)

of 2

XFacebookLinkedIn
Aerospace - ISSN 2226-4310