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Aerospace, Volume 12, Issue 7

July 2025 - 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 C, 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
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Articles (84)

  • Article
  • Open Access
1,676 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...

  • Article
  • Open Access
517 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...

  • Article
  • Open Access
1,643 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...

  • Article
  • Open Access
1,275 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...

  • Article
  • Open Access
780 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...

  • Article
  • Open Access
1,080 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...

  • Article
  • Open Access
1,353 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...

  • Article
  • Open Access
585 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...

  • Article
  • Open Access
543 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...

  • Article
  • Open Access
1 Citations
547 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...

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Aerospace - ISSN 2226-4310