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Aerospace, Volume 9, Issue 2

2022 February - 70 articles

Cover Story: Small satellites and CubeSats are experiencing increasing interest from the space community, because of the performance available with current technologies at a reduced cost with respect to larger spacecraft. Notably, the hardware composing the attitude and orbit control systems has reached a strong maturity level, and the dimensions of the components allow redundant sets of sensors and actuators. Thus, the software shall be able to handle these redundancies with a fault-tolerant structure. This research work develops an attitude and orbit determination system with embedded failure detection and isolation functions, and autonomous redundant component management for on-board failure recovery. The system is sized for small satellites, characterized by very limited computing power. View this paper
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Articles (70)

  • Article
  • Open Access
52 Citations
6,695 Views
27 Pages

21 February 2022

With the development of high-altitude and long-endurance unmanned aerial vehicles (UAVs), optimization of the coordinated energy dispatch of UAVs’ energy management systems has become a key target in the research of electric UAVs. Several diffe...

  • Article
  • Open Access
8 Citations
4,231 Views
19 Pages

21 February 2022

The E-LISA research project, under way within the Clean Sky 2 framework, has the objective of developing an innovative iron bird dedicated to executing tests on the landing gear of a small aircraft transport equipped with an electro-mechanical landin...

  • Article
  • Open Access
10 Citations
4,999 Views
21 Pages

19 February 2022

Based on the technical platform of electrically actuated nose wheel steering systems, a new type of damping shimmy reduction technology is developed to break through the limitations of traditional hydraulic damping shimmy reduction methods, and an el...

  • Article
  • Open Access
9 Citations
6,755 Views
21 Pages

Effectiveness of Conflict Resolution Methods in Air Traffic Management

  • Anrieta Dudoit,
  • Vytautas Rimša,
  • Marijonas Bogdevičius and
  • Jacek Skorupski

19 February 2022

Aircraft fly en route under concurrent event situations (conflicting situations), which occur when they operate in the same airspace but are too close to each other in the same time frame. Hence, the safe horizontal distance between them is not less...

  • Article
  • Open Access
8 Citations
4,097 Views
11 Pages

19 February 2022

The new requirement of installing the flight stabilization system onboard the airplanes for performing the single-pilot flights in IFR rules was issued lately. It caused the necessity of developing such a system for small aircraft. The proposed syste...

  • Article
  • Open Access
6 Citations
6,327 Views
35 Pages

Lessons Learned from IDEASSat: Design, Testing, on Orbit Operations, and Anomaly Analysis of a First University CubeSat Intended for Ionospheric Science

  • Yi-Chung Chiu,
  • Loren C. Chang,
  • Chi-Kuang Chao,
  • Tzu-Ya Tai,
  • Kai-Lun Cheng,
  • Hsin-Tzu Liu,
  • Rong Tsai-Lin,
  • Chi-Ting Liao,
  • Wei-Hao Luo and
  • Mustapha Meftah
  • + 12 authors

18 February 2022

Given the pervasive use of satellite and over the horizon wireless communication technology in modern society, ionospheric disturbances that can disrupt such services are a crucial consideration. Ionospheric irregularities, plasma bubbles and other p...

  • Article
  • Open Access
10 Citations
4,476 Views
23 Pages

17 February 2022

Aircraft trajectory planning is affected by various uncertainties. Among them, those in weather prediction have a large impact on the aircraft dynamics. Trajectory planning that assumes a deterministic weather scenario can cause significant performan...

  • Article
  • Open Access
7 Citations
4,898 Views
31 Pages

16 February 2022

The aerodynamic performance of clap-and-fling mechanism in a KU-Beetle—a tailless two-winged flapping-wing micro air vehicle—was investigated for various horizontal free-stream inflows. Three inflow speeds of 0 (hovering), 2.52 m/s and 5....

  • Article
  • Open Access
10 Citations
3,421 Views
13 Pages

Electro-Thermal Parameters of Graphene Nano-Platelets Films for De-Icing Applications

  • Khitem Lahbacha,
  • Sarah Sibilia,
  • Gianmarco Trezza,
  • Gaspare Giovinco,
  • Francesco Bertocchi,
  • Sergio Chiodini,
  • Francesco Cristiano and
  • Antonio Maffucci

16 February 2022

This paper provides a study of some relevant electro-thermal properties of commercial films made by pressed graphene nano-platelets (GNPs), in view of their use as heating elements in innovative de-icing systems for aerospace applications. The equiva...

  • Article
  • Open Access
5 Citations
2,793 Views
25 Pages

16 February 2022

Rotor-stator cavities are often found in turbomachinery; they supply cold air that is bled from the compressor to the turbine blades. The pressure of the outlet of a rotor-stator cavity is axisymmetric under normal circumstances. However, its pressur...

  • Feature Paper
  • Article
  • Open Access
16 Citations
4,049 Views
16 Pages

TDE-Based Adaptive Integral Sliding Mode Control of Space Manipulator for Space-Debris Active Removal

  • Zhibin Zhang,
  • Xinhong Li,
  • Xun Wang,
  • Xin Zhou,
  • Jiping An and
  • Yanyan Li

16 February 2022

The safe and dependable removal of large-scale space debris has been a long-standing challenge that is critical to the safety of spacecraft and astronauts. In the process of capturing and deorbiting space debris, the space manipulator must achieve ex...

  • Article
  • Open Access
15 Citations
3,568 Views
21 Pages

15 February 2022

The integrated thermal management system of aircraft is essential to maintain a suitable environment for the cabin crew and devices. The system is composed of the air-cycle refrigeration subsystem, the vapor-compression refrigeration subsystem, the l...

  • Article
  • Open Access
7 Citations
7,323 Views
42 Pages

14 February 2022

A concept of a new energy management system synthesizing meteorological and orographic influences on airplane safety envelope was developed and implemented at the ZHAW Centre for Aviation. A corresponding flight simulation environment was built in a...

  • Article
  • Open Access
23 Citations
9,809 Views
18 Pages

14 February 2022

In this study, we developed a new reacting flow solver based on OpenFOAM (OF) and Cantera, with the capabilities of (i) dealing with detailed species transport and chemistry, (ii) integration using a well-balanced splitting scheme, and (iii) two adva...

  • Article
  • Open Access
24 Citations
4,141 Views
17 Pages

14 February 2022

The global path planning of planetary surface rovers is crucial for optimizing exploration benefits and system safety. For the cases of long-range roving or obstacle constraints that are time-varied, there is an urgent need to improve the computation...

  • Article
  • Open Access
5 Citations
6,067 Views
28 Pages

Mission Test Campaign for the EIRSAT-1 Engineering Qualification Model

  • Maeve Doyle,
  • Rachel Dunwoody,
  • Gabriel Finneran,
  • David Murphy,
  • Jack Reilly,
  • Joseph Thompson,
  • Sai Krishna Reddy Akarapu,
  • Joseph Mangan,
  • Sarah Walsh and
  • Lorraine Hanlon
  • + 13 authors

13 February 2022

The compact, standardised form factor of CubeSats allows for the use of commercial off-the-shelf components, reducing traditional barriers to entry, such as cost and development time. More than 1500 of these small spacecraft have been launched in the...

  • Article
  • Open Access
14 Citations
12,568 Views
30 Pages

Thermal Vacuum Test Campaign of the EIRSAT-1 Engineering Qualification Model

  • Rachel Dunwoody,
  • Jack Reilly,
  • David Murphy,
  • Maeve Doyle,
  • Joseph Thompson,
  • Gabriel Finneran,
  • Lána Salmon,
  • Conor O’Toole,
  • Sai Krishna Reddy Akarapu and
  • Sheila McBreen
  • + 16 authors

12 February 2022

CubeSats facilitate rapid development and deployment of missions for educational, technology demonstration, and scientific purposes. However, they are subject to a high failure rate, with a leading cause being the lack of system-level verification. T...

  • Article
  • Open Access
23 Citations
4,530 Views
17 Pages

12 February 2022

The guidance problem of a confrontation between an interceptor, a hypersonic vehicle, and an active defender is investigated in this paper. As a hypersonic multiplayer pursuit-evasion game, the optimal guidance scheme for each adversary in the engage...

  • Article
  • Open Access
2 Citations
4,173 Views
22 Pages

Multi-Objective Comparative Analysis of Active Modular Rectifier Architectures for a More Electric Aircraft

  • Unai Atutxa,
  • Igor Baraia-Etxaburu,
  • Víctor Manuel López,
  • Fernando González-Hernando and
  • Alejandro Rujas

12 February 2022

Aircraft electrification requires reliable, power-dense, high-efficient, and bidirectional rectifiers to improve the overall performance of existing aircrafts. Thus, traditional bulky passive rectifiers must be substituted by active rectifiers, satis...

  • Article
  • Open Access
27 Citations
5,714 Views
28 Pages

Neural Network Prediction for Ice Shapes on Airfoils Using iceFoam Simulations

  • Sergei Strijhak,
  • Daniil Ryazanov,
  • Konstantin Koshelev and
  • Aleksandr Ivanov

12 February 2022

In this article the procedure and method for the ice accretion prediction for different airfoils using artificial neural networks (ANNs) are discussed. A dataset for the neural network is based on the numerical experiment results—obtained throu...

  • Article
  • Open Access
16 Citations
6,359 Views
18 Pages

Design of a Low-Cost Air Bearing Testbed for Nano CMG Maneuvers

  • Charalampos Papakonstantinou,
  • Georgios Moraitis,
  • Vaios Lappas and
  • Vassilis Kostopoulos

12 February 2022

In this paper, a low-cost, miniature spacecraft attitude control simulator is presented for testing miniature actuators such as Nano Control Moment Gyroscopes (CMGs) for simple maneuvers. The experimental setup is composed by an attitude control syst...

  • Article
  • Open Access
20 Citations
4,098 Views
19 Pages

11 February 2022

The formation flight of quadrotor unmanned aerial vehicles (UAVs) is a complex multi-constraint process. When designing a formation controller, the dynamic model of the UAV itself has modeling errors and uncertainties. Model predictive control (MPC)...

  • Article
  • Open Access
13 Citations
4,372 Views
25 Pages

10 February 2022

Meeting the demand with the available airspace capacity is one of the most challenging problems faced by Air Traffic Management. Nowadays, this collaborative Demand–Capacity Balancing process often ends up enforcing Air Traffic Flow Management...

  • Article
  • Open Access
9 Citations
4,615 Views
20 Pages

Characterization of Residual Stresses and Grain Structure in Hot Forging of GH4169

  • Zibiao Wang,
  • Guangsha Hou,
  • Yang Zhao,
  • Jianfei Sun,
  • Jiangzhen Guo and
  • Wuyi Chen

10 February 2022

Residual stresses (RS) in hot forging severely degrade the machining accuracy and stability of super alloy parts. This is the main reason for deformation during subsequent mechanical machining. RS need recognition, as well as the microstructure and p...

  • Review
  • Open Access
88 Citations
21,881 Views
19 Pages

Aircraft 4D Trajectory Prediction in Civil Aviation: A Review

  • Weili Zeng,
  • Xiao Chu,
  • Zhengfeng Xu,
  • Yan Liu and
  • Zhibin Quan

10 February 2022

Aircraft four dimensional (4D, including longitude, latitude, altitude and time) trajectory prediction is a key technology for existing automation systems and the basis for future trajectory-based operations. This paper firstly summarizes the backgro...

  • Article
  • Open Access
10 Citations
5,314 Views
19 Pages

Flocking Bird Strikes on Engine Fan Blades and Their Effect on Rotor System: A Numerical Simulation

  • Bin Wu,
  • Jiewei Lin,
  • Anshun Xie,
  • Ning Wang,
  • Guichang Zhang,
  • Junhong Zhang and
  • Huwei Dai

10 February 2022

Bird strikes are a common, serious, and devastating event in aviation accidents, and multi-bird strikes are also frequently reported. A numerical multi-bird-strike simulation was performed to investigate the effect of flocking birds striking on engin...

  • Article
  • Open Access
6 Citations
8,391 Views
22 Pages

Low Speed Aerodynamic Analysis of the N2A Hybrid Wing–Body

  • Andrea Aprovitola,
  • Francesco Aurisicchio,
  • Pasquale Emanuele Di Nuzzo,
  • Giuseppe Pezzella and
  • Antonio Viviani

10 February 2022

Reduction of atmospheric emissions is currently a mandatory requirement for aircraft manufacturers. Several studies performed on Blended Wing–Body configurations showed a promising capability of reducing fuel consumption by increasing, at the s...

  • Article
  • Open Access
2 Citations
2,678 Views
19 Pages

9 February 2022

Distributed control architecture can bring many benefits to the engine control system, but the delay and packet dropout introduced by network communication will bring negative effects to the control system. The aging and deterioration of the engine a...

  • Article
  • Open Access
14 Citations
3,373 Views
27 Pages

9 February 2022

In this study, numerical simulations were carried out to investigate the flow and heat transfer characteristics of jet array impingement cooling in the quasi-leading-edge channel of gas turbine blades. The influence laws of Reynolds number (Re, 10,00...

  • Article
  • Open Access
72 Citations
6,297 Views
19 Pages

Global Optimization of UAV Area Coverage Path Planning Based on Good Point Set and Genetic Algorithm

  • Jinbiao Yuan,
  • Zhenbao Liu,
  • Yeda Lian,
  • Lulu Chen,
  • Qiang An,
  • Lina Wang and
  • Bodi Ma

7 February 2022

When performing area coverage tasks in some special scenarios, fixed-wing aircraft conventionally adopt the scan-type of path planning, where the distance between two adjacent tracks is usually less than the minimum turning radius of the aircraft. Th...

  • Article
  • Open Access
1 Citations
3,080 Views
22 Pages

Reliability-Oriented Configuration Optimization of More Electrical Control Systems

  • Zirui Liao,
  • Shaoping Wang,
  • Jian Shi,
  • Dong Liu and
  • Rentong Chen

6 February 2022

More electrical vehicles adopt dissimilar redundant control systems with dissimilar power supplies and dissimilar actuators to achieve high reliability and safety, but this introduces more intricacy into the configuration design. Currently, it is dif...

  • Article
  • Open Access
13 Citations
3,510 Views
15 Pages

4 February 2022

The icing phenomenon seriously threatens flight safety, and, therefore, the aircraft needs to be equipped with an icing protection system. Icing may still occur when the anti-icing system is in operation when the protection range or protection power...

  • Article
  • Open Access
6 Citations
3,105 Views
16 Pages

3 February 2022

Stratospheric airships with a solar array have demonstrated overwhelming superiority in many aspects, such as earth observation, meteorological survey, and communication relay. The solar array supplies sufficient power for the airship to be in flight...

  • Article
  • Open Access
12 Citations
4,065 Views
18 Pages

3 February 2022

The present study focuses on producibility and surface roughness characteristics of airfoil geometries and their effect on aerodynamic performance for different velocities, surface roughness values and angles of attack. Two different tray orientation...

  • Article
  • Open Access
7 Citations
3,458 Views
27 Pages

3 February 2022

The pursuit of excellent performance in meta-heuristic algorithms has led to a myriad of extensive and profound research and achievements. Notably, many space mission planning problems are solved with the help of meta-heuristic algorithms, and releva...

  • Article
  • Open Access
1 Citations
2,580 Views
18 Pages

1 February 2022

To solve the issues of directional control and aerodynamic moment coupling for a low-aspect tailless configuration with a diamond-shaped wing, we herein propose the concept of a flow coupling rudder (FCR). The FCR was composed of two basic control su...

  • Article
  • Open Access
2,841 Views
19 Pages

Probabilistic Risk Analysis of Aircraft Self-Collisions: A Case Study

  • Dooyoul Lee,
  • Hwanjeong Cho,
  • Min-Saeng Kim and
  • Kybeom Kwon

1 February 2022

Airborne self-collisions occur primarily in military aircraft because of external stores and are frequently experienced by personnel operating these aircraft. In most cases, objects causing self-collisions are irregularly shaped and unstable. Consequ...

  • Article
  • Open Access
19 Citations
3,074 Views
17 Pages

1 February 2022

The current challenges facing the aerospace domain require unconventional solutions, which could be sought in new configurations of future aircraft and spacecraft. The choice of optimal concepts requires the consideration of a significant amount of c...

  • Article
  • Open Access
20 Citations
5,383 Views
27 Pages

1 February 2022

Evaluating the performance of complex systems, such as air traffic management (ATM), is a challenging task. When regarding aviation as a time-continuous system measured in value-discrete time series via performance indicators and certain metrics, it...

  • Article
  • Open Access
9 Citations
6,819 Views
25 Pages

Factors Impacting Chinese and European Vertical Fight Efficiency

  • Judith Rosenow,
  • Gong Chen,
  • Hartmut Fricke and
  • Yanjun Wang

1 February 2022

Increasing complexity due to a constantly growing number of target functions turns air traffic trajectory optimization into a multidimensional and nonlinear task that in turn necessitates a focus on the case-sensitive most important criteria. The cri...

  • Article
  • Open Access
3 Citations
3,409 Views
28 Pages

30 January 2022

This study investigated the variation of the osculating orbit elements of a spacecraft propelled by photonic laser propulsion (PLP) under the two-body problem assumption. The PLP thrusting system can produce continuous and constant thrust. This paper...

  • Article
  • Open Access
25 Citations
6,064 Views
22 Pages

28 January 2022

Climate change currently taking place around the world requires humanity to take decisive action. One way, as envisaged in the European Green Deal, is to reduce the emissions of harmful chemical compounds of the transport sector by 90% by 2050. This...

  • Article
  • Open Access
14 Citations
5,318 Views
19 Pages

28 January 2022

To examine the plasma-assisted combustion of a scramjet, a microwave-enhanced gliding arc plasma method was proposed in this study, and the flame structure and combustion instability were observed. The mechanism of plasma-assisted combustion was obta...

  • Article
  • Open Access
49 Citations
15,080 Views
26 Pages

Advanced Sizing Methodology for a Multi-Mode eVTOL UAV Powered by a Hydrogen Fuel Cell and Battery

  • Jae-Hyun An,
  • Do-Youn Kwon,
  • Kwon-Su Jeon,
  • Maxim Tyan and
  • Jae-Woo Lee

27 January 2022

A critical drawback of battery-powered eVTOL UAVs is their limited range and endurance, and this drawback could be solved by using a combination of hydrogen fuel cells and batteries. The objective of this paper is to develop a sizing methodology for...

  • Article
  • Open Access
25 Citations
6,135 Views
28 Pages

A Numerical Study on Aircraft Noise Mitigation Using Porous Stator Concepts

  • Christopher Teruna,
  • Leandro Rego,
  • Damiano Casalino,
  • Daniele Ragni and
  • Francesco Avallone

27 January 2022

This manuscript presents the application of a recently developed noise reduction technology, constituted by poro-serrated stator blades on a full-scale aircraft model, in order to reduce rotor-stator interaction noise in the fan stage. This study was...

  • Article
  • Open Access
10 Citations
4,700 Views
17 Pages

26 January 2022

The maximum contact force is one of the most important indicators for contact problems. In this paper, the configuration optimization is conducted to reduce the maximum contact force for a free-floating space robot capturing tumbling target. First, t...

  • Article
  • Open Access
32 Citations
8,304 Views
38 Pages

Initial Assessment of a Fuel Cell—Gas Turbine Hybrid Propulsion Concept

  • Arne Seitz,
  • Markus Nickl,
  • Florian Troeltsch and
  • Kathrin Ebner

26 January 2022

A fuel cell—gas turbine hybrid propulsion concept is introduced and initially assessed. The concept uses the water mass flow produced by a hydrogen fuel cell in order to improve the efficiency and power output of the gas turbine engine through...

  • Article
  • Open Access
17 Citations
7,083 Views
18 Pages

Design of an ATC Tool for Conflict Detection Based on Machine Learning Techniques

  • Javier Alberto Pérez-Castán,
  • Luis Pérez-Sanz,
  • Lidia Serrano-Mira,
  • Francisco Javier Saéz-Hernando,
  • Irene Rodríguez Gauxachs and
  • Víctor Fernando Gómez-Comendador

26 January 2022

Given the ongoing interest in the application of Machine Learning (ML) techniques, the development of new Air Traffic Control (ATC) tools is paramount for the improvement of the management of the air transport system. This article develops an ATC too...

  • Article
  • Open Access
10 Citations
3,760 Views
16 Pages

Plasma Assisted Re-Ignition of Aeroengines under High Altitude Conditions

  • Ghazanfar Mehdi,
  • Sara Bonuso and
  • Maria Grazia De Giorgi

26 January 2022

Re-ignition of aeroengines under high altitude conditions is of great importance to the safety and use of lean-burn flame. This study is focused on the experimental and numerical characterization of flow dynamics and flame re-ignition in a rectangula...

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Aerospace - ISSN 2226-4310