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Aerospace, Volume 11, Issue 6

June 2024 - 86 articles

Cover Story: UAVs need to traverse multiple essential target points in the shortest possible time in smart city and modern military scenarios. Such missions require UAVs to improve mission execution efficiency by optimizing trajectories. Multi-waypoint trajectory optimization is one of the key technologies for UAVs to perform this kind of complex task, and this paper discusses this technical field in depth, covering the core contents of trajectory planning and time optimization. By adopting the advanced Constrained Parameterized Differential Dynamic Programming (C-PDDP) algorithm, the UAV is able to optimize the flight time of each trajectory segment while meeting the path constraints, which significantly shortens the mission time and improves mission efficiency. View this paper
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Articles (86)

  • Article
  • Open Access
3 Citations
3,292 Views
22 Pages

Effects of Leading Edge Radius on Stall Characteristics of Rotor Airfoil

  • Simeng Jing,
  • Guoqing Zhao,
  • Yuan Gao and
  • Qijun Zhao

The effects of leading edge radius on the static and dynamic stall characteristics of rotor airfoils are investigated. Initially, a parametric airfoil (PARFOIL) method is employed to generate four morphed airfoils with different leading edge radii ba...

  • Article
  • Open Access
7 Citations
1,626 Views
20 Pages

In this work, we examine the possibility of converting a light propeller-driven aircraft, powered by a spark-ignition, reciprocating piston, and internal combustion engine running on AVGAS, into one powered by an electric motor driven by a proton exc...

  • Article
  • Open Access
2 Citations
3,215 Views
19 Pages

In the last decades, electromechanical actuators started to be introduced in transport aircraft for primary and secondary flight control surfaces. Some innovative architectures have been proposed in the literature to use these actuators for high-lift...

  • Article
  • Open Access
1 Citations
1,470 Views
12 Pages

The health assessment of airborne lithium batteries is crucial for flight testing, ensuring the safety and reliability of aircraft power systems. This paper proposes a support vector machine-based algorithm for the health assessment of airborne lithi...

  • Article
  • Open Access
3 Citations
2,577 Views
16 Pages

In a satellite-denied environment, a swarm of drones is capable of achieving relative positioning and navigation by leveraging the high-precision ranging capabilities of the inter-drone data link. However, because of factors such as high drone mobili...

  • Article
  • Open Access
7 Citations
5,667 Views
31 Pages

Experimental Pressure Gain Analysis of Pulsed Detonation Engine

  • Alina Bogoi,
  • Tudor Cuciuc,
  • Andrei Vlad Cojocea,
  • Mihnea Gall,
  • Ionuț Porumbel and
  • Constantin Eusebiu Hrițcu

A pulsed detonation chamber (PDC) equipped with Hartmann–Sprenger resonators has been designed and tested for both Hydrogen/air and Hydrogen/Oxygen mixtures. A full-factorial experimental campaign employing four factors with four levels each ha...

  • Article
  • Open Access
3 Citations
1,765 Views
19 Pages

Numerical Investigation of Model Support, Closed Engine Nacelle and Scale Effect on a Wind Tunnel Test Model

  • Ioan-Laurentiu Padureanu,
  • Dumitru Pepelea,
  • Gilbert Stoican,
  • Marco Marini,
  • Nicole Viola and
  • Matthew Clay

In the frame of the H2020 MORE&LESS project co-funded by European Commission, a test campaign for a hypersonic vehicle demonstrator took place at the INCAS Trisonic Facility. CFD analysis was used to quantify the effects of the wind tunnel model...

  • Article
  • Open Access
2 Citations
2,068 Views
28 Pages

To enhance the performance of rigid coaxial rotors across both hovering and high-speed cruising conditions, this study develops a novel aerodynamic optimization method that differentiates between the upper and lower rotors. Utilizing the lifting line...

  • Article
  • Open Access
2 Citations
2,113 Views
18 Pages

This paper introduces a new type of flexible rudder surface based on the cosine-type zero Poisson’s ratio honeycomb to enhance the adaptive capabilities of aircraft and enable multi-condition, rudderless flight. The zero Poisson’s ratio h...

  • Article
  • Open Access
2 Citations
1,634 Views
26 Pages

An Adaptive Similar Scenario Matching Method for Predicting Aircraft Taxiing Time

  • Peiran Qiao,
  • Minghua Hu,
  • Jianan Yin,
  • Jiaming Su,
  • Yutong Chen and
  • Mengxuan Yin

Accurate prediction of taxiing time is important in ensuring efficient and safe operations on the airport surface. It helps improve ground operation efficiency, reduce fuel waste, and improve carbon emissions at the airport. In actual operations, tax...

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Aerospace - ISSN 2226-4310