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Aerospace, Volume 9, Issue 7

2022 July - 63 articles

Cover Story: Venusian clouds are conjectured to be a possible habitat for life. We propose a mission to explore the clouds of Venus to evaluate their habitability and to search for signs of life. The spacecraft would launch from Earth with an orbiter and a probe carrying an aerobot. A super-pressure balloon would cycle at altitudes between 48 and 60 km using a combination of ballast drop, gas venting, and the thermal effects of the environment. The gondola design is derived from the Pioneer Venus Large Probe pressure vessel. The aerobot would transmit data via orbiter relay combined with a direct-to-Earth link. The proposed mission could help to elucidate the limits of habitability and the role of unknown chemistry or the possibly life itself in the atmosphere of Venus. View this paper
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Articles (63)

  • Article
  • Open Access
21 Citations
6,169 Views
15 Pages

Flight Departure Time Prediction Based on Deep Learning

  • Hang Zhou,
  • Weicong Li,
  • Ziqi Jiang,
  • Fanger Cai and
  • Yuting Xue

Accurate flight departure time prediction enables the rational use of airport support resources, aprons, and runway resources, and promotes the implementation of collaborative decision-making. In order to accurately predict the flight departure time,...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
18 Citations
4,184 Views
29 Pages

Despite offering often significant advantages with respect to other flying machines, especially in terms of flight endurance, airships are typically harder to control. Technological solutions borrowed from the realm of shipbuilding, such as bow thrus...

(This article belongs to the Special Issue Mission Analysis and Design of Lighter-than-Air Flying Vehicles)
  • Article
  • Open Access
15 Citations
3,442 Views
25 Pages

Reliability estimation for key components of a mechanical system is of great importance in prognosis and health management in aviation industry. Both degradation data and failure time data contain abundant reliability information from different sourc...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
19 Citations
5,074 Views
14 Pages

A multiple-airport system (MAS) consists of more than two airports in a metropolitan area under a large block of terminal airspace that is managed by one or two air traffic control units. When the capacity of an airport or of the terminal airspace dr...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
2,711 Views
17 Pages

Planetary rovers play a critical role in space exploration missions, where one of the most fundamental algorithms is pose determination. Due to environmental and computational constraints, real-time pose determinations of planetary rovers can only us...

(This article belongs to the Special Issue Recent Advances in Spacecraft Dynamics and Control)
  • Article
  • Open Access
2 Citations
3,685 Views
20 Pages

Airport management plays a key role in the air traffic system. Introducing resources at the right time can minimize the effects of disruptions, reduce delays, and save costs as well as optimize the carbon footprint of the airport. Efficient decision-...

(This article belongs to the Special Issue Advances in Air Traffic and Airspace Control and Management)
  • Article
  • Open Access
6 Citations
3,006 Views
18 Pages

Accurately identifying the peak value of impact load acting on the helicopter structure during weapon launch is of great significance to the design and finalization of weapon pylons. Firstly, a method of standardized preprocessing load signal is prop...

(This article belongs to the Special Issue Structural Dynamics and Control)
  • Article
  • Open Access
11 Citations
3,077 Views
15 Pages

As the key mechanism of attitude control of micro/nano-satellites, the flywheel design is mostly based on empirical formulae that do not meet the requirements of lightweight and high-performance micro/nano-satellite platforms. In this paper, the stru...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
7 Citations
5,967 Views
20 Pages

Variable diameter rotor can improve the flight performance of the aircraft both in hovering and forward flying and a duct can improve the rotor performance further both in force and efficiency. In previous studies, those two parts are always studied...

(This article belongs to the Section Aeronautics)
  • Communication
  • Open Access
41 Citations
16,025 Views
9 Pages

Venus Life Finder Missions Motivation and Summary

  • Sara Seager,
  • Janusz J. Petkowski,
  • Christopher E. Carr,
  • David H. Grinspoon,
  • Bethany L. Ehlmann,
  • Sarag J. Saikia,
  • Rachana Agrawal,
  • Weston P. Buchanan,
  • Monika U. Weber and
  • on behalf of the Venus Life Finder Mission Team
  • + 4 authors

Finding evidence of extraterrestrial life would be one of the most profound scientific discoveries ever made, advancing humanity into a new epoch of cosmic awareness. The Venus Life Finder (VLF) missions feature a series of three direct atmospheric p...

(This article belongs to the Special Issue The Search for Signs of Life on Venus: Science Objectives and Mission Designs)
  • Article
  • Open Access
3 Citations
2,936 Views
19 Pages

The velocity and acceleration of geostationary transfer orbit (GTO) satellites change dramatically and periodically, and the operating area extends from hundreds of kilometers to 36,000 km above the Earth’s surface. This leads to the limitation...

  • Article
  • Open Access
17 Citations
7,279 Views
24 Pages

Trajectory optimization has been an active area of research for air transport studies for several decades. But almost all flight optimizers proposed in the literature remain close-sourced, which presents a major disadvantage for the advancement of sc...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
2 Citations
3,340 Views
24 Pages

Shape Optimisation of Assembled Plate Structures with the Boundary Element Method

  • Llewellyn Morse,
  • Vincenzo Mallardo,
  • Zahra Sharif-Khodaei and
  • Ferri M.H. Aliabadi

A novel methodology is presented for performing sensitivity analyses of assembled plate structures using the Boundary Element Method (BEM). The main novelty of this work is that the exact implicit derivatives of the BEM formulations for assembled pla...

(This article belongs to the Special Issue Recent Advances in Computational Mechanics)
  • Article
  • Open Access
36 Citations
11,783 Views
18 Pages

Design and Analysis of MataMorph-3: A Fully Morphing UAV with Camber-Morphing Wings and Tail Stabilizers

  • Peter L. Bishay,
  • James S. Kok,
  • Luis J. Ferrusquilla,
  • Brian M. Espinoza,
  • Andrew Heness,
  • Antonio Buendia,
  • Sevada Zadoorian,
  • Paul Lacson,
  • Jonathan D. Ortiz and
  • Daniel Olvera
  • + 1 author

Conventional aircraft use discrete flight control surfaces to maneuver during flight. The gaps and discontinuities of these control surfaces generate drag, which degrades aerodynamic and power efficiencies. Morphing technology aims to replace convent...

(This article belongs to the Special Issue Advances in Aerospace Sciences and Technology III)
  • Article
  • Open Access
13 Citations
5,852 Views
17 Pages

Conceptual Research on a Mono-Biplane Aerodynamics-Driven Morphing Aircraft

  • Tingyu Guo,
  • Liangtao Feng,
  • Chenhua Zhu,
  • Xiaopeng Zhou and
  • Haixin Chen

The operation of aircrafts with high aspect ratio wings is usually vulnerable to low-standard airports and bad weather. A new concept for a mono-biplane aerodynamics-driven morphing aircraft is proposed. The movable and fixed wings form a biplane mod...

(This article belongs to the Special Issue Advances in Aerospace Sciences and Technology III)
  • Article
  • Open Access
8 Citations
5,589 Views
15 Pages

Flow Feature in Supersonic Non-Isobaric Jet near the Nozzle Edge

  • Valeriy Zapryagaev,
  • Ivan Kavun and
  • Nikolay Kiselev

Using the example of studying the supersonic underexpanded jet initial section, the issue of interpreting the experimental visualization data and Pitot pressure measurement data using the results of numerical calculations (2d RANS k-ω SST) is d...

(This article belongs to the Special Issue Jet Flow Analysis)
  • Article
  • Open Access
8 Citations
5,192 Views
30 Pages

A coupled aerostructural aircraft design and trajectory optimization framework is developed for the Air Cargo Challenge competition to maximize the expected score based on cargo carried, altitude achieved and distance traveled. Its modular architectu...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
9 Citations
4,336 Views
17 Pages

This work addresses the problem of vertical wind profile online estimation at a given location. Specifically, the north and east components of the wind are continuously estimated as functions of time and altitude at two waypoints used for landing on...

(This article belongs to the Special Issue Advances in Air Traffic and Airspace Control and Management)
  • Article
  • Open Access
1 Citations
5,062 Views
24 Pages

The Stability Analysis of a Tether for a Segmented Space Elevator

  • Shihao Luo,
  • Naigang Cui,
  • Xiaowei Wang,
  • Youhua Fan and
  • Haitao Gu

The space elevator system is a space tether system used to solve low-cost space transportation. Its high efficiency, large load and other characteristics have broad application prospects in the aerospace field. The stability analysis is the foundatio...

(This article belongs to the Section Astronautics & Space Science)
  • Communication
  • Open Access
18 Citations
7,448 Views
17 Pages

Design Principles for a Contrail-Minimizing Trial in the North Atlantic

  • Jarlath Molloy,
  • Roger Teoh,
  • Seán Harty,
  • George Koudis,
  • Ulrich Schumann,
  • Ian Poll and
  • Marc E. J. Stettler

The aviation industry has committed to decarbonize its CO2 emissions. However, there has been much less industry focus on its non-CO2 emissions, despite recent studies showing that these account for up to two-thirds of aviation’s climate impact...

(This article belongs to the Special Issue Aircraft Emissions and Climate Impact)
  • Article
  • Open Access
7 Citations
4,675 Views
14 Pages

Numerical Solution for the Single-Impulse Flyby Co-Orbital Spacecraft Problem

  • Haoxiang Su,
  • Zhenghong Dong,
  • Lihao Liu and
  • Lurui Xia

The traversal inspection of satellites in satellite constellations or geosynchronous orbits has been a focus of research. A large number of variable orbit requirements in the “single-to-single” mode severely affects the efficiency of insp...

(This article belongs to the Collection Space Systems Dynamics)
  • Article
  • Open Access
3 Citations
5,192 Views
26 Pages

This paper proposed a multi-view surface array to enlarge the field-of-view (FOV) from 45° × 45° to 72° × 75° and improve the estimation precision of guidance information. First, based on circular and rectangular FOV senso...

  • Article
  • Open Access
4 Citations
3,252 Views
25 Pages

In aerospace engineering, high-order computational fluid dynamics (CFD) solvers suitable for three-dimensional unstructured meshes are less developed than expected. The Runge–Kutta discontinuous Galerkin (RKDG) finite element method with compac...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
7 Citations
10,018 Views
21 Pages

Analysis of Bilateral Air Services Agreement Liberalization in Australia

  • Iryna Heiets,
  • Richard C.K. Yeun,
  • Wim J.C. Verhagen and
  • Jiezhuoma La

This paper examines an assessment of the level of air transport services liberalization in Australia in order to generate recommendations on what key market access features of Air Services Agreements should be revised to reflect the changes in air tr...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
17 Citations
6,081 Views
18 Pages

Object detection is a fundamental part of computer vision, with a wide range of real-world applications. It involves the detection of various objects in digital images or video. In this paper, we propose a proof of concept usage of computer vision al...

(This article belongs to the Special Issue Applications of Drones)
  • Article
  • Open Access
4 Citations
3,161 Views
29 Pages

To improve the resolution and accuracy of the high-order weighted compact nonlinear scheme (WCNS), a new ϵ-adaptive algorithm based on local smoothness indicators is proposed. The new algorithm introduces a high-order global smoothness indicato...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
7 Citations
3,554 Views
18 Pages

The hardware-in-the-loop (HIL) simulation is an important approach to test space robotic operations, rendering virtual free-floating dynamics on robotic facilities. However, this approach suffers from velocity divergence due to intrinsic time delay i...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
3,070 Views
24 Pages

A complex command and control task was selected as the test task, which included observing the overall and local situation, the interactive operation and situation display of detection equipment, the erection and launch of air defense equipment, and...

  • Review
  • Open Access
20 Citations
5,368 Views
12 Pages

Supersonic Combustion Modeling and Simulation on General Platforms

  • Shizhuo Huang,
  • Qian Chen,
  • Yuwei Cheng,
  • Jinyu Xian and
  • Zhengqi Tai

Supersonic combustion is an advanced technology for the next generation of aerospace vehicles. In the last two decades, numerical simulation has been widely used for the investigation on supersonic combustion. In this paper, the modeling and simulati...

(This article belongs to the Special Issue Supersonic and Hypersonic Transportation Systems)
  • Article
  • Open Access
9 Citations
5,744 Views
26 Pages

Design and Analysis of a Novel Floating Docking Mechanism for On-Orbit Refueling

  • Zhicheng Sun,
  • Shipeng Li,
  • Huan Zhang,
  • Haiming Lei and
  • Xiaodong Song

The docking mechanism is a key component for on-orbit refueling technology. In this paper, the design and analysis of a novel floating docking mechanism for on-orbit berthing-based refueling is presented. Compared with traditional berthing and dockin...

(This article belongs to the Special Issue Recent Advances in Spacecraft Dynamics and Control)
  • Article
  • Open Access
10 Citations
3,759 Views
15 Pages

Multisatellite Task Allocation and Orbit Planning for Asteroid Terminal Defence

  • Yuelong Luo,
  • Xiuqiang Jiang,
  • Suchuan Zhong,
  • Yuandong Ji and
  • Guohao Sun

Near-Earth asteroids are a great threat to the Earth, especially potential rendezvous and collision asteroids. To protect the Earth from an asteroid collision, it is necessary to investigate the asteroid defence problem. An asteroid terminal defence...

(This article belongs to the Special Issue Recent Advances in Spacecraft Dynamics and Control)
  • Article
  • Open Access
14 Citations
5,031 Views
14 Pages

Aerial Platform Design Options for a Life-Finding Mission at Venus

  • Weston P. Buchanan,
  • Maxim de Jong,
  • Rachana Agrawal,
  • Janusz J. Petkowski,
  • Archit Arora,
  • Sarag J. Saikia,
  • Sara Seager,
  • James Longuski and
  • on behalf of the Venus Life Finder Mission Team

Mounting evidence of chemical disequilibria in the Venusian atmosphere has heightened interest in the search for life within the planet’s cloud decks. Balloon systems are currently considered to be the superior class of aerial platform for exte...

(This article belongs to the Special Issue The Search for Signs of Life on Venus: Science Objectives and Mission Designs)
  • Review
  • Open Access
38 Citations
8,027 Views
35 Pages

A Survey of Precision Formation Relative State Measurement Technology for Distributed Spacecraft

  • Zhang Zhang,
  • Lei Deng,
  • Jiaqi Feng,
  • Liang Chang,
  • Dong Li and
  • Yilin Qin

High-precision relative-state measurement technology is one of the key technologies for achieving the precision formation flying of distributed spacecraft. This paper conducts a comprehensive analysis of the precision formation-flying projects of dis...

(This article belongs to the Section Astronautics & Space Science)
  • Review
  • Open Access
82 Citations
17,376 Views
22 Pages

A Review of Spatial Robotic Arm Trajectory Planning

  • Ye Dai,
  • Chaofang Xiang,
  • Yuan Zhang,
  • Yupeng Jiang,
  • Wenyin Qu and
  • Qihao Zhang

With space technology development, the spatial robotic arm plays an increasingly important role in space activities. Spatial robotic arms can effectively replace humans to complete in-orbit service tasks. The trajectory planning is the basis of robot...

(This article belongs to the Special Issue Recent Advances in Spacecraft Dynamics and Control)
  • Article
  • Open Access
7 Citations
3,117 Views
21 Pages

This paper proposes a novel fully nonlinear refined beam element for pre-twisted structures undergoing large deformation and finite untwisting. The present model is constructed in the twisted basis to account for the effects of geometrical nonlineari...

  • Article
  • Open Access
18 Citations
7,874 Views
16 Pages

Mission Architecture to Characterize Habitability of Venus Cloud Layers via an Aerial Platform

  • Rachana Agrawal,
  • Weston P. Buchanan,
  • Archit Arora,
  • Athul P. Girija,
  • Maxim De Jong,
  • Sara Seager,
  • Janusz J. Petkowski,
  • Sarag J. Saikia,
  • Christopher E. Carr and
  • on behalf of Venus Life Finder Mission Team
  • + 2 authors

Venus is known for its extreme surface temperature and its sulfuric acid clouds. But the cloud layers on Venus have similar temperature and pressure conditions to those on the surface of Earth and are conjectured to be a possible habitat for microsco...

(This article belongs to the Special Issue The Search for Signs of Life on Venus: Science Objectives and Mission Designs)
  • Article
  • Open Access
36 Citations
7,573 Views
17 Pages

The Investigation of Plume-Regolith Interaction and Dust Dispersal during Chang’E-5 Descent Stage

  • Haiyan Zhang,
  • Cunhui Li,
  • Jilin You,
  • Xiaoping Zhang,
  • Yi Wang,
  • Liping Chen,
  • Qingfei Fu,
  • Baogui Zhang and
  • Yuming Wang

The plume-surface interaction that occurs as a result of a variable-thrust engine exhaust plume impinging on soil during landings is critical for future lunar mission design. Unique lunar environmental properties, such as low gravity, high vacuum, an...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
3 Citations
2,666 Views
16 Pages

Dynamic identification of the intensity of the moving loads applied to structures is an important task in aerospace, marine, and transportation industries. In the present work, a general technique is presented for identification of the time variation...

(This article belongs to the Special Issue Recent Advances in Computational Mechanics)
  • Article
  • Open Access
11 Citations
3,396 Views
25 Pages

Fixed-Time Circular Impact-Time Guidance with Look Angle Constraint

  • Xiangxiang Li,
  • Wanchun Chen,
  • Zhongyuan Chen,
  • Ting Wang and
  • Heng Shi

A fixed-time nonlinear circular guidance law that satisfies the impact time constraint is proposed. By utilizing the geometric principle that the length of a circular arc connecting the missile and the target can be analytically calculated, the exact...

  • Review
  • Open Access
24 Citations
14,596 Views
47 Pages

Aircraft Emissions, Their Plume-Scale Effects, and the Spatio-Temporal Sensitivity of the Atmospheric Response: A Review

  • Kieran N. Tait,
  • Mohammad Anwar H. Khan,
  • Steve Bullock,
  • Mark H. Lowenberg and
  • Dudley E. Shallcross

Non-CO2 aircraft emissions are responsible for the majority of aviation’s climate impact, however their precise effect is largely dependent on the environmental conditions of the ambient air in which they are released. Investigating the princip...

(This article belongs to the Special Issue Aircraft Emissions and Climate Impact)
  • Article
  • Open Access
4 Citations
6,449 Views
16 Pages

This paper analyses a new half-bridge current–source inverter for avionic systems. In the circuit, two 28 V batteries are used as inputs. These voltage sources are connected to inductors which create a constant current source. Then only two hig...

(This article belongs to the Special Issue New Trends in Aviation Development 2021-2022)
  • Article
  • Open Access
4 Citations
2,821 Views
18 Pages

Adaptive Local Maximum-Entropy Surrogate Model and Its Application to Turbine Disk Reliability Analysis

  • Jiang Fan,
  • Qinghao Yuan,
  • Fulei Jing,
  • Hongbin Xu,
  • Hao Wang and
  • Qingze Meng

The emerging Local Maximum-Entropy (LME) approximation, which combines the advantages of global and local approximations, has an unsolved issue wherein it cannot adaptively change the morphology of the basis function according to the local characteri...

(This article belongs to the Special Issue Application of Multidisciplinary Optimization and Artificial Intelligence Techniques to Aerospace Engineering)
  • Article
  • Open Access
10 Citations
2,913 Views
22 Pages

Incremental Backstepping Sliding-Mode Trajectory Control for Tailless Aircraft with Stability Enhancer

  • Zihou He,
  • Jianbo Hu,
  • Yingyang Wang,
  • Jiping Cong,
  • Linxiao Han and
  • Maoyu Su

This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control of a tailless aircraft with unknown disturbances and model uncertainties. The proposed controller is based on a nonlinear dynamic model of the taille...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
5 Citations
4,404 Views
20 Pages

Some asteroids flying close to Earth may pose a threat of impact. Among them, the structural and dynamical characteristics of rubble-pile asteroids can be changed because of the tidal force of the Earth in this process. This can provide key informati...

(This article belongs to the Special Issue Recent Advances in Spacecraft Dynamics and Control)
  • Article
  • Open Access
5 Citations
4,906 Views
15 Pages

Accurate identification of electrical load working status can provide information support to the remote electrical distribution system (EDS) of more electric aircraft (MEA), which could use it to realize redundant switching and protection. This paper...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
11 Citations
12,263 Views
31 Pages

Retrofitting Cost Modeling in Aircraft Design

  • Pierluigi Della Vecchia,
  • Massimo Mandorino,
  • Vincenzo Cusati and
  • Fabrizio Nicolosi

Aircraft retrofitting is a challenging task involving multiple scenarios and stakeholders. Providing a strategy to retrofit an existing platform needs detailed knowledge of multiple aspects, ranging from aircraft performance and emissions, developmen...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
12 Citations
6,496 Views
22 Pages

Waverider is a hypersonic vehicle that improves the lift-to-drag ratio using the shockwave attached to the leading edge of the lifting surface. Owing to its superior aerodynamic performance, it exhibits a viable external configuration in hypersonic f...

(This article belongs to the Special Issue Hypersonics: Emerging Research)
  • Article
  • Open Access
6 Citations
2,945 Views
23 Pages

There has been a concern that the accurate numerical simulation of multi-body flow, which is caused by the multiple disintegrations of expired spacecraft re-entering into the near space, has a critical bottleneck impact on the falling area of the dis...

  • Article
  • Open Access
4 Citations
3,124 Views
16 Pages

This paper researches the parametric optimization of a two-stage transonic compressor having a large air bypass at partial rotating speed according to flow analysis for a turbine-based combined cycle engine (TBCC). To obtain adequate thrust, the inle...

(This article belongs to the Special Issue Fluid Flow Mechanics (2nd Edition))
  • Article
  • Open Access
1 Citations
3,463 Views
27 Pages

Layout Design and Verification of a Space Payload Distributed Capture and Lock System

  • Gang Wang,
  • Yimeng Yao,
  • Jingtian Wang,
  • Weiye Huo,
  • Guosheng Xu and
  • Xi Hu

In this paper, the mechanism scheme and parametric design of a capture and lock system are studied based on the high reliability of locking systems. By analyzing the workflow and boundary conditions of the capture and lock system, a positioning desig...

(This article belongs to the Section Astronautics & Space Science)

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Aerospace - ISSN 2226-4310