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Aerospace, Volume 9, Issue 6

June 2022 - 52 articles

Cover Story: The use of EMAs for aeronautical applications promises substantial benefits regarding efficiency and operability. To advance the design of power electronics and secondary power supply, there is a strong need for the ability to swiftly study the effects of mission and operational aspects on actuator energy consumption. Pursuant to this, a generic mission-level flight control surface EMA power consumption simulation framework is presented. The core of the framework comprises physics-based EMA power estimators, linked with a six-degree-of-freedom flight dynamics and control simulation module. The developed framework could aid in the selection of the actuator, as well as in the optimization of airborne electronics and secondary power supply. View this paper
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Articles (52)

  • Article
  • Open Access
12 Citations
3,769 Views
15 Pages

The vibration characteristics of a composite fan blade are much more complex than those of a solid titanium fan blade due to the anisotropic material properties and complex excitations coming from unsteady flow and mechanically induced vibration. In...

  • Article
  • Open Access
4 Citations
2,824 Views
23 Pages

In recent years, the penetration of low-cost air-launched vehicles for nano/micro satellites has significantly increased worldwide. Conceptual design and overall parameters optimization of the air-launched vehicle has become an exigent task. In the p...

  • Article
  • Open Access
28 Citations
5,726 Views
18 Pages

Space debris severely threatens the safety of spacecraft in near-earth orbit. Dragging space debris into the atmosphere to burn is an effective way to remove it. In this paper, the authors focus on capturing irregular and rotating debris via a flexib...

  • Article
  • Open Access
64 Citations
12,137 Views
20 Pages

Parrot Mambo mini-drone is a readily available commercial quadrotor platform to understand and analyze the behavior of a quadrotor both in indoor and outdoor applications. This study evaluates the performance of three alternative controllers on a Par...

  • Article
  • Open Access
9 Citations
5,645 Views
20 Pages

Development of POLON—A Green Microsatellite Propulsion Module Utilizing 98% Hydrogen Peroxide

  • Jakub Gramatyka,
  • Przemysław Paszkiewicz,
  • Damian Grabowski,
  • Adrian Parzybut,
  • Daria Bodych,
  • Krzysztof Wróblewski,
  • Paweł Surmacz and
  • Krzysztof Pietrzak

The following paper presents the key design and test activities associated with the development of POLON—a green microsatellite propulsion module using 98% Hydrogen Peroxide (HTP). POLON, which stands for “Polish Propulsion Module”,...

  • Article
  • Open Access
7 Citations
4,890 Views
17 Pages

Nonlinear Control of a Single Tail Tilt Servomotor Tri-Rotor Ducted VTOL-UAV

  • Yanpeng Hu,
  • Jin Guo,
  • Pei Ying,
  • Guannan Zeng and
  • Nanyu Chen

This paper explores a novel single tail tilt servomotor tri-rotor ducted vertical takeoff and landing unmanned aerial vehicle system (VTOL-UAV), and proposes a compound control method combining disturbance observer, model predictive control (MPC) and...

  • Article
  • Open Access
5 Citations
2,722 Views
18 Pages

Vibration-based damage assessment technology is a hot topic in aerospace engineering, civil engineering, and mechanical engineering. In this paper, a damage assessment approach using multiple-stage dynamic flexibility analysis is proposed for structu...

  • Review
  • Open Access
37 Citations
8,189 Views
32 Pages

Deep reinforcement learning (DRL) has been widely adopted recently for its ability to solve decision-making problems that were previously out of reach due to a combination of nonlinear and high dimensionality. In the last few years, it has spread in...

  • Article
  • Open Access
7 Citations
3,752 Views
17 Pages

Influence of Mass Flow Rate on the Atomization Characteristics of Screw Conveyor Swirl Injectors

  • Xianggeng Wei,
  • Yiming Feng,
  • Jinying Ye,
  • Na Li and
  • Oskar J. Haidn

This study conducted cold flow experimental research on the influence of mass flow rate on the atomization characteristics of screw conveyer swirl injectors in an opening environment. The Phase Doppler Particle Analyzer (PDPA) and high-speed photogra...

  • Article
  • Open Access
5 Citations
3,622 Views
15 Pages

Simultaneous Pressure and Displacement Measurement on Helicopter Rotor Blades Using a Binocular Stereophotogrammetry PSP System

  • Chunhua Wei,
  • Chenglin Zuo,
  • Xianhui Liao,
  • Guoshuai Li,
  • Lingrui Jiao,
  • Di Peng and
  • Lei Liang

A simultaneous surface pressure and displacement measurement method that integrates pressure-sensitive paint (PSP) and binocular stereophotogrammetry is proposed. The assays were completed on the Φ4 m rotor test stand at China Aerodynamic Researc...

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Aerospace - ISSN 2226-4310