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  Subjects -> AERONAUTICS AND SPACE FLIGHT (Total: 124 journals)
Showing 1 - 30 of 30 Journals sorted alphabetically
Acta Astronautica     Hybrid Journal   (Followers: 236)
Advances in Aerospace Engineering     Open Access   (Followers: 77)
Advances in Aerospace Science and Technology     Open Access   (Followers: 16)
Advances in Astronautics Science and Technology     Hybrid Journal   (Followers: 3)
Advances in Space Research     Hybrid Journal   (Followers: 302)
Aeronautical Journal, The     Hybrid Journal   (Followers: 12)
Aerospace     Open Access   (Followers: 68)
Aerospace Medicine and Human Performance     Full-text available via subscription   (Followers: 25)
Aerospace Science and Technology     Hybrid Journal   (Followers: 318)
Aerospace Systems     Hybrid Journal   (Followers: 11)
Aerospace technic and technology     Open Access   (Followers: 8)
Aerotecnica Missili & Spazio : Journal of Aerospace Science, Technologies & Systems     Hybrid Journal   (Followers: 7)
AIAA Journal     Hybrid Journal   (Followers: 1021)
Air Force Magazine     Full-text available via subscription   (Followers: 11)
Air Medical Journal     Hybrid Journal   (Followers: 7)
Aircraft Engineering and Aerospace Technology     Hybrid Journal   (Followers: 149)
Artificial Satellites     Open Access   (Followers: 22)
ASTRA Proceedings     Open Access   (Followers: 3)
Astrodynamics     Hybrid Journal   (Followers: 5)
Aviation     Open Access   (Followers: 13)
Aviation in Focus - Journal of Aeronautical Sciences     Open Access   (Followers: 7)
Aviation Psychology and Applied Human Factors     Hybrid Journal   (Followers: 27)
Aviation Week     Full-text available via subscription   (Followers: 427)
Canadian Aeronautics and Space Journal     Full-text available via subscription   (Followers: 32)
CEAS Aeronautical Journal     Hybrid Journal   (Followers: 31)
Chinese Journal of Aeronautics     Open Access   (Followers: 20)
Ciencia y Poder Aéreo     Open Access   (Followers: 4)
Civil Aviation High Technologies     Open Access   (Followers: 7)
Control Systems     Hybrid Journal   (Followers: 245)
Cosmic Research     Hybrid Journal   (Followers: 6)
Egyptian Journal of Remote Sensing and Space Science     Open Access   (Followers: 26)
Fatigue of Aircraft Structures     Open Access   (Followers: 22)
Frontiers in Aerospace Engineering     Open Access   (Followers: 21)
Frontiers in Astronomy and Space Sciences     Open Access   (Followers: 16)
Gyroscopy and Navigation     Hybrid Journal   (Followers: 192)
IEEE Aerospace and Electronic Systems Magazine     Full-text available via subscription   (Followers: 263)
IEEE Journal on Miniaturization for Air and Space Systems     Hybrid Journal   (Followers: 3)
IEEE Transactions on Aerospace and Electronic Systems     Hybrid Journal   (Followers: 294)
IEEE Transactions on Circuits and Systems I: Regular Papers     Hybrid Journal   (Followers: 44)
International Journal of Aeroacoustics     Hybrid Journal   (Followers: 38)
International Journal of Aerodynamics     Hybrid Journal   (Followers: 47)
International Journal of Aeronautical and Space Sciences     Hybrid Journal   (Followers: 5)
International Journal of Aerospace Engineering     Open Access   (Followers: 88)
International Journal of Aerospace Innovations     Full-text available via subscription   (Followers: 24)
International Journal of Aerospace Psychology     Hybrid Journal   (Followers: 23)
International Journal of Aerospace Sciences     Open Access   (Followers: 38)
International Journal of Applied Geospatial Research     Hybrid Journal   (Followers: 8)
International Journal of Aviation Management     Hybrid Journal   (Followers: 6)
International Journal of Aviation Technology, Engineering and Management     Full-text available via subscription   (Followers: 8)
International Journal of Aviation, Aeronautics, and Aerospace     Open Access   (Followers: 10)
International Journal of Crashworthiness     Hybrid Journal   (Followers: 11)
International Journal of Micro Air Vehicles     Open Access   (Followers: 12)
International Journal of Satellite Communications Policy and Management     Hybrid Journal   (Followers: 16)
International Journal of Space Science and Engineering     Hybrid Journal   (Followers: 13)
International Journal of Space Structures     Full-text available via subscription   (Followers: 20)
International Journal of Space Technology Management and Innovation     Full-text available via subscription   (Followers: 11)
International Journal of Sustainable Aviation     Hybrid Journal   (Followers: 6)
Investigación Pecuaria     Open Access   (Followers: 2)
Journal of Aerodynamics     Open Access   (Followers: 27)
Journal of Aeronautical Materials     Open Access   (Followers: 10)
Journal of Aerospace Engineering     Full-text available via subscription   (Followers: 67)
Journal of Aerospace Engineering & Technology     Full-text available via subscription   (Followers: 23)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 28)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 57)
Journal of Aerospace Technology and Management     Open Access   (Followers: 11)
Journal of Aircraft     Hybrid Journal   (Followers: 278)
Journal of Aircraft and Spacecraft Technology     Open Access   (Followers: 17)
Journal of Airline and Airport Management     Open Access   (Followers: 12)
Journal of Astrobiology & Outreach     Open Access   (Followers: 6)
Journal of Aviation Technology and Engineering     Open Access   (Followers: 11)
Journal of Aviation/Aerospace Education & Research     Open Access   (Followers: 3)
Journal of Engineering and Technological Sciences     Open Access   (Followers: 3)
Journal of Guidance, Control, and Dynamics     Hybrid Journal   (Followers: 179)
Journal of KONBiN     Open Access   (Followers: 5)
Journal of Navigation     Hybrid Journal   (Followers: 189)
Journal of Propulsion and Power     Hybrid Journal   (Followers: 580)
Journal of Space Safety Engineering     Hybrid Journal   (Followers: 9)
Journal of Space Weather and Space Climate     Open Access   (Followers: 31)
Journal of Spacecraft and Rockets     Hybrid Journal   (Followers: 713)
Journal of Spatial Science     Hybrid Journal   (Followers: 5)
Journal of the American Helicopter Society     Full-text available via subscription   (Followers: 10)
Journal of the Astronautical Sciences     Hybrid Journal   (Followers: 12)
Journal of the Australasian Society of Aerospace Medicine     Open Access   (Followers: 3)
Journal of Wind Engineering and Industrial Aerodynamics     Hybrid Journal   (Followers: 22)
Life Sciences in Space Research     Hybrid Journal   (Followers: 6)
MAD - Magazine of Aviation Development     Open Access   (Followers: 3)
Mekanika : Jurnal Teknik Mesin i     Open Access   (Followers: 1)
Microgravity Science and Technology     Hybrid Journal   (Followers: 4)
New Space     Hybrid Journal   (Followers: 7)
Nonlinear Dynamics     Hybrid Journal   (Followers: 20)
npj Microgravity     Open Access   (Followers: 4)
Open Aerospace Engineering Journal     Open Access   (Followers: 4)
Perspectives of Earth and Space Scientists i     Open Access   (Followers: 2)
Population Space and Place     Hybrid Journal   (Followers: 11)
Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa / Problems of Mechatronics. Armament, Aviation, Safety Engineering     Open Access   (Followers: 4)
Proceedings of the Human Factors and Ergonomics Society Annual Meeting     Hybrid Journal   (Followers: 19)
Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering     Hybrid Journal   (Followers: 43)
Progress in Aerospace Sciences     Full-text available via subscription   (Followers: 83)
Propulsion and Power Research     Open Access   (Followers: 90)
REACH - Reviews in Human Space Exploration     Full-text available via subscription   (Followers: 5)
Research & Reviews : Journal of Space Science & Technology     Full-text available via subscription   (Followers: 21)
RocketSTEM     Free   (Followers: 7)
Russian Aeronautics (Iz VUZ)     Hybrid Journal   (Followers: 24)
Science and Education : Scientific Publication of BMSTU     Open Access   (Followers: 2)
Space and Polity     Hybrid Journal   (Followers: 7)
Space Policy     Hybrid Journal   (Followers: 31)
Space Research Today     Full-text available via subscription   (Followers: 44)
Space Safety Magazine     Free   (Followers: 51)
Space Science International     Open Access   (Followers: 129)
Space Science Reviews     Hybrid Journal   (Followers: 93)
SpaceNews     Free   (Followers: 796)
Spatial Information Research     Hybrid Journal   (Followers: 2)
Transactions on Aerospace Research     Open Access   (Followers: 2)
Transport and Aerospace Engineering     Open Access   (Followers: 4)
Transportmetrica A : Transport Science     Hybrid Journal   (Followers: 8)
Unmanned Systems     Hybrid Journal   (Followers: 5)
Xibei Gongye Daxue Xuebao / Journal of Northwestern Polytechnical University     Open Access   (Followers: 1)
Вісник Національного Авіаційного Університету     Open Access   (Followers: 1)

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International Journal of Micro Air Vehicles
Journal Prestige (SJR): 0.368
Citation Impact (citeScore): 1
Number of Followers: 12  

  This is an Open Access Journal Open Access journal
ISSN (Print) 1756-8293 - ISSN (Online) 1756-8307
Published by Sage Publications Homepage  [1174 journals]
  • Wind tunnel tests of a wing at all angles of attack

    • Authors: Ziqing Ma, Ewoud J.J. Smeur, Guido C.H.E. de Croon
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      Tailsitters have complex aerodynamics that make them hard to control throughout the entire flight envelope, especially at very high angle of attack (AoA) and reverse flow conditions. The development of controllers for these vehicles is hampered by the absence of publicly available data on forces and moments experienced in such conditions. In this paper, wind tunnel experiments are performed under different flap deflections and throttle settings at all possible AoA. The dataset is made open access. Our analysis of the data shows for the tested wing, flap deflections greatly affect the lift coefficient and stall occurs at [math] AoA as well as [math]. Wing-propeller interaction is studied by analyzing the propeller induced force in the axis orthogonal to the thrust axis, which is dependent on AoA, airspeed, flap deflections and thrust in a nonlinear and coupled manner. The influence of inverse flow on the wing is also discussed: The data confirm that when the airflow over the wing is reversed, flap deflections will affect the pitch moment in an opposite way compared to the non-reversed case, but this opposite effect can be avoided by increasing the throttle setting. The data show the exact relationship between flap deflections and forces in this condition. Moreover, it is found that the flap control effectiveness for a wing with or without spinning propellers is usually higher around zero degrees AoA than at [math] and it is more effective to change the flaps from [math] to [math] than from [math] to the respective [math].
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-07-06T01:38:57Z
      DOI: 10.1177/17568293221110931
      Issue No: Vol. 14 (2022)
  • Analyzing visual imagery for emergency drone landing on unknown

    • Authors: Oghuz Bektash, Jacob Juul Naundrup, Anders la Cour-Harbo
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      Autonomous landing is a fundamental aspect of drone operations which is being focused upon by the industry, with ever-increasing demands on safety. As the drones are likely to become indispensable vehicles in near future, they are expected to succeed in automatically recognizing a landing spot from the nearby points, maneuvering toward it, and ultimately, performing a safe landing. Accordingly, this paper investigates the idea of vision-based location detection on the ground for an automated emergency response system which can continuously monitor the environment and spot safe places when needed. A convolutional neural network which learns from image-based feature representation at multiple scales is introduced. The model takes the ground images, assign significance to various aspects in them and recognize the landing spots. The results provided support for the model, with accurate classification of ground image according to their visual content. They also demonstrate the feasibility of computationally inexpensive implementation of the model on a small computer that can be easily embedded on a drone.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-06-30T06:31:23Z
      DOI: 10.1177/17568293221106492
      Issue No: Vol. 14 (2022)
  • Editorial

    • Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.

      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-06-24T06:09:00Z
      DOI: 10.1177/17568293221104967
      Issue No: Vol. 14 (2022)
  • Design optimization-under-uncertainty of a forward swept wing unmanned
           aerial vehicle using SAMURAI

    • Authors: Jolan Wauters
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      In this paper the design optimization-under-uncertainty of a forward swept wing (FSW) blended wing body (BWB) unmanned aerial vehicle (UAV) is examined. Conventional BWBs are often tailless, which leads to a backward swept wing to ensure longitudinal static stability. This in turn can induce flow separation at the tip, leading to a loss of lift, controllability and the appearance of a nose-up pitching moment. A possible solution to this problem is a conceptual redesign by introducing a forward swept wing, which is inherently free of tip-stall, but needs a careful design in order to be controllable. However, fixed wing UAVs are often produced by means of direct injection expanded foam moulding, which is characterized by not negligible production tolerances. This lead to a reliability-based robust design optimization problem, for which a novel framework is employed: SAMURAI. Firstly, the method accounts for computational cost by means of surrogate modelling, an analytical treatment of the problem and an asynchronous updating scheme that balances design space exploration and objective exploitation. Secondly, the method treats the problem as a multi-objective problem, which leads to a Pareto front of robust and reliable designs. The result is a novel series of UAV designs that are inherently free of tip stall, perform robustly and meet the stability requirements with the target reliability obtained with a computationally feasible budget.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-05-11T07:36:58Z
      DOI: 10.1177/17568293221092139
      Issue No: Vol. 14 (2022)
  • Dynamic Modeling and Control Law Design of a Fuel-electric Hybrid
           Multi-rotor UAV

    • Authors: Xice Xu, Yang Lu, Xufeng Wu
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      In this paper, the design of control law for a new concept fuel-electric hybrid multi-rotor UAV with lift/attitude control separation is investigated. The remarkable feature of the UAV is that it has a large proportion of fuel weight. Firstly, based on the quasi-coordinate Lagrangian equation and sloshing equivalent model using the multi-mass-spring analogy, the non-linear dynamic model of the UAV considering the fuel slosh dynamics is established. Compared with the existing multi-rotor modeling method, it is more intuitive and accurate to describe the non-linear coupling process of sloshing and UAV's motion degrees of freedom. Secondly, the attitude control law is designed based on the finite-time sliding mode observer and cascaded continuous sliding mode controller to eliminate the adverse effects of fuel sloshing and mass changing, and only using the measurable angles. Furthermore, aiming at the problem of power redundancy of the altitude channel, a memoryless non-linear altitude authority assignment controller based on vertical acceleration is proposed for improving the control performance. Finally, the simulation results of the waypoint flight illustrate the feasibility and effectiveness of the proposed control strategy.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-02-15T05:46:23Z
      DOI: 10.1177/17568293221078925
      Issue No: Vol. 14 (2022)
  • On association of lift generation, wake topology and kinematics of
           oscillating foils

    • Authors: Suyash Verma, Muhammad S.U. Khalid, Arman Hemmati
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      The association of lift generation and evolution of wake topology behind an oscillating foil with combined heaving and pitching motion is investigated numerically at a range of bluereduced frequency (0.16 [math] 0.48), phase offset (0[math] [math] 315[math]) and Reynolds number (1000 [math] 4000). The pitch-dominated kinematics that coincide with the range of [math] 120[math] and [math] 225[math] suggests that leading edge vortices are suppressed while trailing edge vortices dominate the wake with increasing reduced frequency. This corresponds to a transition in wake topology from a [math] to a reverse Von Kármán wake mode. Contrarily, heave dominated kinematics (120[math] [math] 225[math]) did not exhibit any wake topology transition with increasing [math]. The temporal lift variation associated with heave-dominated regime further revealed a symmetric feature in terms of the time taken to attain peak lift generation within an oscillation cycle. This temporal symmetry was, however, lost as kinematics transitioned from heave- to pitch-dominated regime. Analyzing the wake evolution and lift features at quarter phase of an oscillation cycle revealed the existence of a correspondence between the two processes during the heave- and pitch-dominated kinematics.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-24T01:04:37Z
      DOI: 10.1177/17568293211073959
      Issue No: Vol. 14 (2022)
  • Aeroacoustic optimization of MAV rotors

    • Authors: Pietro Li Volsi, David Gomez-Ariza, Romain Gojon, Thierry Jardin, Jean-Marc Moschetta
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      The more restrictive airspace regulations force drone manufacturers to take into account the noise emitted by the drone during the design phase, along with its aerodynamic performance to increase the flight time. A Non-Linear Vortex Lattice Method (NVLM), coupled with the Farassat Formulation-1A of the Ffowcs-Williams and Hawkings acoustic analogy is used to evaluate the aerodynamic and aeroacoustic performance of MAV rotors. Pymoo, a Python-based optimization framework, is employed to modify the geometry, evaluate its performance and extract the set of Pareto optimal solutions. The two objectives are the aerodynamic Figure-of-Merit and the Sound Pressure Level of the Blade Passing Frequency tone for a microphone located at a far-field distance of 1.62 m and 30[math] below the rotor plane. The approach proposed in this paper takes into account up to ten different parameters, ranging from the twist and chord distributions, to the rake and skew angles.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-24T01:04:07Z
      DOI: 10.1177/17568293211070827
      Issue No: Vol. 14 (2022)
  • Nonlinear model predictive control for improving range-based relative
           localization by maximizing observability

    • Authors: Shushuai Li, Christophe De Wagter, Guido C. H. E. de Croon
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      Wireless ranging measurements have been proposed for enabling multiple Micro Air Vehicles (MAVs) to localize with respect to each other. However, the high-dimensional relative states are weakly observable due to the scalar distance measurement. Hence, the MAVs have degraded relative localization and control performance under unobservable conditions as can be deduced by the Lie derivatives. This paper presents a nonlinear model predictive control (NMPC) by maximizing the determinant of the observability matrix to generate optimal control inputs, which also satisfy constraints including multi-robot tasks, input limitation, and state bounds. Simulation results validate the localization and control efficacy of the proposed MPC method for range-based multi-MAV systems with weak observability, which has faster convergence time and more accurate localization compared to previously proposed random motions. A real-world experiment on two Crazyflies indicates the optimal states and control behaviours generated by the proposed NMPC.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-21T12:41:33Z
      DOI: 10.1177/17568293211073680
      Issue No: Vol. 14 (2022)
  • Extended incremental non-linear control allocation (XINCA) for quadplanes

    • Authors: H.J. Karssies, C. De Wagter
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      Hybrid UAVs have gained a lot of interest for their combined vertical take-off & landing (VTOL) and efficient forward flight capabilities. But their control is facing challenges in over-actuation and conflicting requirements depending on the flight phase which can easily lead to actuator saturation. Incremental Non-linear Control Allocation (INCA) has been proposed to solve the platform’s control allocation problem in the case of saturation or over-actuation by minimizing a set of objective functions. This work demonstrates INCA on quadplanes, an in-plane combination between a quadrotor and a conventional fixed-wing, and proposes an extension to control the outer loop. The novel controller is called Extended INCA (XINCA) and adds the wing orientation as a force-generating actuator in the outerloop control optimization. This leads to a single controller for all flight phases that avoids placing the wing at negative angles of attack and minimizes the load on hover motors. XINCA has low dependence on accurate vehicle models and requires only several optimization parameters. Flight simulations and experimental flights are performed to demonstrate the performance.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-21T12:41:14Z
      DOI: 10.1177/17568293211070825
      Issue No: Vol. 14 (2022)
  • An implementation framework for vision-based bat-like inverted perching
           with bi-directionalthrust quadrotor

    • Authors: Pengfei Yu, KC Wong
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      This paper presents an implementation framework to perform a vision-guided, bat-like inverted perching maneuver with a bi-directional thrust quadrotor platform. The framework consists of several distinct modules (guidance, motion planning, control, state estimation) that can be easily be individually customized in the future to meet specific research requirements. The main contribution of this paper lies in the whole framework pipeline with a modular structure developed for implementing a generalized framework for an agile quadrotor to achieve inverted perching. A computationally-light guidance module has been developed as an example to demonstrate the capability while being independent of accurate pre-known target information, and does not require the state estimation of the quadrotor to be provided by an external motion capture system as in our previous work. A motion planning module based on an optimization method has been introduced to generate a two-stage inverted perching trajectory aiming at minimizing altitude loss during the half-flip maneuver. A control module has been developed to enable a bi-directional quadrotor to fly in both upright and inverted states and closely follow the intended trajectory. The compensation strategy used in the control module is key to minimizing the transition time between the upright and inverted states. Finally, an experimental flight platform has been developed to demonstrate the capabilities of the framework. During testing, the proposed framework has achieved an 80 % success rate. To the best of our knowledge, this paper presents the first time a quadrotor has achieved the inverted perching maneuver using onboard vision guidance.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-18T11:56:06Z
      DOI: 10.1177/17568293211073672
      Issue No: Vol. 14 (2022)
  • Estimating wind using a quadrotor

    • Authors: Gautier Hattenberger, Murat Bronz, Jean-Philippe Condomines
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      The aim of this work is to estimate the average wind influencing a quadrotor drone only based on standard navigation sensors and equations of motion. It can be used in several situation, including atmospheric studies, trajectory planning under environmental constraints, or as a reference for studying flights in shear layer. For this purpose, a small quadrotor drone with spherical shape has been developed. Flight data are recorded from telemetry during indoor and outdoor flight tests and are post-processed. The proposed solution is based on a calibration procedure with global optimization to extract the drag model and a Kalman Filter for online estimation of the wind speed and direction. Finally, an on-board implementation of the real-time estimation is demonstrated with real flights in controlled indoor environment.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-13T01:05:53Z
      DOI: 10.1177/17568293211070824
      Issue No: Vol. 14 (2022)
  • Field report: Deployment of a fleet of drones for cloud exploration

    • Authors: Gautier Hattenberger, Titouan Verdu, Nicolas Maury, Pierre Narvor, Fleur Couvreux, Murat Bronz, Simon Lacroix, Grègoire Cayez, Gregory C. Roberts
      Abstract: International Journal of Micro Air Vehicles, Volume 14, Issue , January-December 2022.
      Drones are commonly used for civil applications and are accessible to those with limited piloting skills in several scenarios. However, the deployment of a fleet in the context of scientific research can lead to complex situations that require an important preparation in terms of logistics, permission to fly from authorities, and coordination during the flights. This paper is a field report of the flight campaign held at the Barbados Island as part of the NEPHELAE project. The main objectives were to fly into trade wind cumulus clouds to understand the microphysical processes involved in their evolution, as well as to provide a proof of concept of sensor-based adaptive navigation patterns to optimize the data collection. After introducing the flight strategy and context of operation, the main challenges and the solutions to address them will be presented, to conclude with the evaluation of some technical evolution developed from these experiments.
      Citation: International Journal of Micro Air Vehicles
      PubDate: 2022-01-10T01:30:02Z
      DOI: 10.1177/17568293211070830
      Issue No: Vol. 14 (2022)
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