Log in

Relevant bibliographies by topics / Flight in formation / Journal articles

To see the other types of publications on this topic, follow the link: Flight in formation.

Journal articles on the topic 'Flight in formation'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 journal articles for your research on the topic 'Flight in formation.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse journal articles on a wide variety of disciplines and organise your bibliography correctly.

1

Verhagen, Collin MA, Hendrikus G. Visser, and Bruno F. Santos. "A decentralized approach to formation flight routing of long-haul commercial flights." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 8 (2018): 2992–3004. http://dx.doi.org/10.1177/0954410018791068.

Full text

Abstract:

This paper describes the development of an optimization-based cooperative planning system for the efficient routing and scheduling of extended flight formations. This study considers the use of formation flight as a means to reduce the overall fuel consumption in long-haul airline operations. It elaborates on the operational implementation of formation flight, particularly focusing on the formation flight routing. A completely decentralized approach is presented, in the sense that formation flight is not planned pre-flight and is not subjected to any predefined routing restrictions. A greedy c

APA, Harvard, Vancouver, ISO, and other styles

2

Gosiewski, Zdzisław, and Leszek Ambroziak. "UAV Autonomous Formation Flight Experiment with Virtual Leader Control Structure." Solid State Phenomena 198 (March 2013): 254–59. http://dx.doi.org/10.4028/www.scientific.net/ssp.198.254.

Full text

Abstract:

The problem of autonomous formation flight control of UAVs (Unmanned Aerial Vehicles) is presented in the paper. A decentralized control method of the autonomous formation flight realization is described. A practical approach to the UAV formation flight control was shown. The applied method bases on the information exchange between flying objects. The shared data concern the position and velocity of the aircraft. Constructed UAV airframe was presented as well as used autopilot, developed formation flight control unit, wireless communication links and used data packet structure. The main aim of

APA, Harvard, Vancouver, ISO, and other styles

3

Weihua, Zhao, and Tiauw Hiong Go. "Robust Decentralized Formation Flight Control." International Journal of Aerospace Engineering 2011 (2011): 1–13. http://dx.doi.org/10.1155/2011/157590.

Full text

Abstract:

Motivated by the idea of multiplexed model predictive control (MMPC), this paper introduces a new framework for unmanned aerial vehicles (UAVs) formation flight and coordination. Formulated using MMPC approach, the whole centralized formation flight system is considered as a linear periodic system with control inputs of each UAV subsystem as its periodic inputs. Divided into decentralized subsystems, the whole formation flight system is guaranteed stable if proper terminal cost and terminal constraints are added to each decentralized MPC formulation of the UAV subsystem. The decentralized robu

APA, Harvard, Vancouver, ISO, and other styles

4

Kazimierczak, Roman, Wiesław Milewski, Zdzisław Gosiewski, Leszek Ambroziak, and Cezary Kownacki. "Towards implementation of a formation flying for efficient UAV operations." Journal of KONBiN 48, no. 1 (2018): 399–417. http://dx.doi.org/10.2478/jok-2018-0063.

Full text

Abstract:

Abstract A flight of a UAV formation is an efficient way to implement surveillance and reconnaissance operations. The usage of a few UAVs as a formation instead of a single vehicle allows creating a distributed network of sensors, which decreases the duration of flight missions and enlarges a total field of view. From a practical point of view, implementations of formation flights require taking into account several separate aspects of flight of UAV such as a quick take-off of several aircraft, aggregating all UAVs in the same space to create swarm and collective flight of the formation toward

APA, Harvard, Vancouver, ISO, and other styles

5

Gu, Yu, Giampiero Campa, and Mario Innocenti. "Formation Flight Control." International Journal of Aerospace Engineering 2011 (2011): 1–2. http://dx.doi.org/10.1155/2011/798981.

Full text

APA, Harvard, Vancouver, ISO, and other styles

6

Marks, Tobias, Katrin Dahlmann, Volker Grewe, et al. "Climate Impact Mitigation Potential of Formation Flight." Aerospace 8, no. 1 (2021): 14. http://dx.doi.org/10.3390/aerospace8010014.

Full text

Abstract:

The aerodynamic formation flight, which is also known as aircraft wake-surfing for efficiency (AWSE), enables aircraft to harvest the energy inherent in another aircraft’s wake vortex. As the thrust of the trailing aircraft can be reduced during cruise flight, the resulting benefit can be traded for longer flight time, larger range, less fuel consumption, or cost savings accordingly. Furthermore, as the amount and location of the emissions caused by the formation are subject to change and saturation effects in the cumulated wake of the formation can occur, AWSE can favorably affect the climate

APA, Harvard, Vancouver, ISO, and other styles

7

Marks, Tobias, Katrin Dahlmann, Volker Grewe, et al. "Climate Impact Mitigation Potential of Formation Flight." Aerospace 8, no. 1 (2021): 14. http://dx.doi.org/10.3390/aerospace8010014.

Full text

Abstract:

The aerodynamic formation flight, which is also known as aircraft wake-surfing for efficiency (AWSE), enables aircraft to harvest the energy inherent in another aircraft’s wake vortex. As the thrust of the trailing aircraft can be reduced during cruise flight, the resulting benefit can be traded for longer flight time, larger range, less fuel consumption, or cost savings accordingly. Furthermore, as the amount and location of the emissions caused by the formation are subject to change and saturation effects in the cumulated wake of the formation can occur, AWSE can favorably affect the climate

APA, Harvard, Vancouver, ISO, and other styles

8

Almeida, Marcelo Furtado de, and Fábio Angioluci Diniz Campos. "Carga de trabalho de instrutores da AFA durante uma instrução de formatura na aeronave T-27." Revista da UNIFA 37 (September 20, 2024): 1–16. https://doi.org/10.22480/rev.unifa.2024.37.616.

Full text

Abstract:

The high cognitive demand inherent in flying is identified as a fundamental factor contributing substantially to pilots’ workload (WL). This WL, in turn, impacts fatigue, performance, and flight safety. The proposed study aims to evaluate the WL of military flight instructors. Delving into the conceptualization and measurement of WL, the study acknowledges its subjective nature, influenced by various dimensions. The research was conducted with 22 flight instructors from the Air Force Academy (AFA), focusing on formation flights. Methodological procedures included the use of the NASA-TLX questi

APA, Harvard, Vancouver, ISO, and other styles

9

Hartjes, Sander, Hendrikus G. Visser, and Marco E. G. van Hellenberg Hubar. "Trajectory Optimization of Extended Formation Flights for Commercial Aviation." Aerospace 6, no. 9 (2019): 100. http://dx.doi.org/10.3390/aerospace6090100.

Full text

Abstract:

This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircraft can attain an appreciable reduction in induced drag and associated reduction in fuel burn by flying in the upwash of the lead aircraft’s wake. In the present study, a previously developed multi-phase optimal control (MOC) framework for the synthesis of two-ship flight formations has been extended

APA, Harvard, Vancouver, ISO, and other styles

10

Bangash, Z. A., R. P. Sanchez, A. Ahmed, and M. J. Khan. "Aerodynamics of Formation Flight." Journal of Aircraft 43, no. 4 (2006): 907–12. http://dx.doi.org/10.2514/1.13872.

Full text

APA, Harvard, Vancouver, ISO, and other styles

11

Pachter, Meir, John J. D’Azzo, and Andrew W. Proud. "Tight Formation Flight Control." Journal of Guidance, Control, and Dynamics 24, no. 2 (2001): 246–54. http://dx.doi.org/10.2514/2.4735.

Full text

APA, Harvard, Vancouver, ISO, and other styles

12

Pachter, M., J. J. D'Azzo, and J. L. Dargan. "Automatic formation flight control." Journal of Guidance, Control, and Dynamics 17, no. 6 (1994): 1380–83. http://dx.doi.org/10.2514/3.21364.

Full text

APA, Harvard, Vancouver, ISO, and other styles

13

MITANI, Shinji, Toru YAMAMOTO, Isao KAWANO, Shin-ichiro SAKAI, Hiroshi TSUNEMI, and FFAST Team. "FFAST: Formation Flight All Sky Telescope, Formation Flight System Analysis and Design." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 8, ists27 (2010): Td_7—Td_15. http://dx.doi.org/10.2322/tastj.8.td_7.

Full text

APA, Harvard, Vancouver, ISO, and other styles

14

Martinez-Ponce, Joseph, Brenden Herkenhoff, Ahmed Aboelezz, et al. "Studies on V-Formation and Echelon Flight Utilizing Flapping-Wing Drones." Drones 8, no. 8 (2024): 395. http://dx.doi.org/10.3390/drones8080395.

Full text

Abstract:

V-Formation and echelon formation flights can be seen used by migratory birds throughout the year and have left many scientists wondering why they choose very specific formations. Experiments and analytical studies have been completed on the topic of the formation flight of birds and have shown that migratory birds benefit aerodynamically by using these formations. However, many of these studies were completed using fixed-wing models, while migratory birds both flap and glide while in formation. This paper reports the design of and experiments with a flapping-wing model rather than only a fixe

APA, Harvard, Vancouver, ISO, and other styles

15

Kwon, Daniel W. "Propellantless formation flight applications using electromagnetic satellite formations." Acta Astronautica 67, no. 9-10 (2010): 1189–201. http://dx.doi.org/10.1016/j.actaastro.2010.06.042.

Full text

APA, Harvard, Vancouver, ISO, and other styles

16

Antczak, Adam, Maciej Lasek, and Krzysztof Sibilski. "Efficient Positioning of Two Long-Range Passenger Aircraft in Formation Flight." Transactions on Aerospace Research 22, no. 3 (2022): 21–31. http://dx.doi.org/10.2478/tar-2022-0014.

Full text

Abstract:

Abstract In today’s world, each airline is forced to look for new savings opportunities. One of the methods may be the use of formation flights in daily flight operations, which may allow a reduction in fuel consumption by several percentages. The paper presents the genesis of how the consideration of such flights and the possibility of their implementation in an airline had started. The leader’s plane generates vortices, which, with the proper alignment of the planes to one another, can reduce the drag on the wingman. However, the wrong position may not only have no positive effect but also m

APA, Harvard, Vancouver, ISO, and other styles

17

Zhang, Dong, Yong Chen, Xinmin Dong, Zongcheng Liu, and Yang Zhou. "Numerical Aerodynamic Characteristics Analysis of the Close Formation Flight." Mathematical Problems in Engineering 2018 (August 29, 2018): 1–13. http://dx.doi.org/10.1155/2018/3136519.

Full text

Abstract:

The aerodynamic characteristics of the close formation flight are numerically analyzed to facilitate a greater understanding of the vortex effects between UAVs and technically support the application of close formation flight for UAVs. The aerodynamic characteristics of a single UAV are calculated, the results of which are used as the reference to the variation of aerodynamic values in the comparison with close formation flight. The vortex effects of the leading UAV on the aerodynamic characteristics of the trailing UAV in the two UAV close formation flight are analyzed. The position where the

APA, Harvard, Vancouver, ISO, and other styles

18

Voskuijl, Mark. "Cruise Range in Formation Flight." Journal of Aircraft 54, no. 6 (2017): 2184–91. http://dx.doi.org/10.2514/1.c034246.

Full text

APA, Harvard, Vancouver, ISO, and other styles

19

Jongho Shin and H. J. Kim. "Nonlinear Model Predictive Formation Flight." IEEE Transactions on Systems, Man, and Cybernetics - Part A: Systems and Humans 39, no. 5 (2009): 1116–25. http://dx.doi.org/10.1109/tsmca.2009.2021935.

Full text

APA, Harvard, Vancouver, ISO, and other styles

20

Rayner, Jeremy M. V. "Fat and formation in flight." Nature 413, no. 6857 (2001): 685–86. http://dx.doi.org/10.1038/35099643.

Full text

APA, Harvard, Vancouver, ISO, and other styles

21

Weimerskirch, Henri, Julien Martin, Yannick Clerquin, Peggy Alexandre, and Sarka Jiraskova. "Energy saving in flight formation." Nature 413, no. 6857 (2001): 697–98. http://dx.doi.org/10.1038/35099670.

Full text

APA, Harvard, Vancouver, ISO, and other styles

22

Kentfield, J. A. C. "Formation Flight and Much More." AIAA Journal 45, no. 8 (2007): 1795–97. http://dx.doi.org/10.2514/1.31222.

Full text

APA, Harvard, Vancouver, ISO, and other styles

23

Sumano, E., R. Castro, R. Lozano, and S. Salazar. "Synchronized Flight Formation of Quadrotors*." IFAC Proceedings Volumes 46, no. 30 (2013): 345–51. http://dx.doi.org/10.3182/20131120-3-fr-4045.00042.

Full text

APA, Harvard, Vancouver, ISO, and other styles

24

Doty, St B. "Space Flight and Bone Formation." Materialwissenschaft und Werkstofftechnik 35, no. 12 (2004): 951–61. http://dx.doi.org/10.1002/mawe.200400840.

Full text

APA, Harvard, Vancouver, ISO, and other styles

25

Ghommem, M., and V. M. Calo. "Flapping wings in line formation flight: a computational analysis." Aeronautical Journal 118, no. 1203 (2014): 485–501. http://dx.doi.org/10.1017/s0001924000009325.

Full text

Abstract:

AbstractThe current understanding of the aerodynamics of birds in formation flights is mostly based on field observations. The interpretation of these observations is usually made using simplified aerodynamic models. Here, we investigate the aerodynamic aspects of formation flights. We use a potential flow solver based on the unsteady vortex lattice method (UVLM) to simulate the flow over flapping wings flying in grouping arrangements and in proximity of each other. UVLM has the capability to capture unsteady effects associated with the wake. We demonstrate the importance of properly capturing

APA, Harvard, Vancouver, ISO, and other styles

26

Meng, Guang Lei. "Control Architecture and Control Laws Design for Multiple UAVs Formation Flight." Applied Mechanics and Materials 246-247 (December 2012): 853–57. http://dx.doi.org/10.4028/www.scientific.net/amm.246-247.853.

Full text

Abstract:

An autonomous formation-flight method for multiple UAVs (Unmanned Aerial Vehicle) was designed. First the mathematical representation of formation shape was analyzed. Then the control architecture was devised for multiple UAVs formation flight based on finite state machine. The flight states of the wing UAV were built through the formation flight and the transformation relationships of these flight states were defined. So the automated transformation among these flight states could be achieved and the intelligence of the pilots could be mimicked by this way. Aiming at the typical flight state

APA, Harvard, Vancouver, ISO, and other styles

27

Ye Yan, Chao Li, and Yue-neng Yang. "Simulation on Spacecraft Formation Flight and Formation Reconfiguration." MATEC Web of Conferences 160 (2018): 05011. http://dx.doi.org/10.1051/matecconf/201816005011.

Full text

Abstract:

Spacecraft formation flight refers to two or more spacecraft according to a certain formation or arrangement of flight, it has important application value for deep spatial exploration, spatial science experiment, ground investigation and military and so. This paper studies the spacecraft formation flight design and formation reconfiguration based on STK. Firstly, the Clohessy-Wiltshire (CW) equation is used to describe the relative motion of the near-circular orbit and deduce the relative orbital dynamics model. Then, based on the dynamic method of the CW equation, the spatial circular formati

APA, Harvard, Vancouver, ISO, and other styles

28

Zhan, Guang, Zheng Gong, Quanhui Lv, et al. "Flight Test of Autonomous Formation Management for Multiple Fixed-Wing UAVs Based on Missile Parallel Method." Drones 6, no. 5 (2022): 99. http://dx.doi.org/10.3390/drones6050099.

Full text

Abstract:

This paper reports on the formation and transformation of multiple fixed-wing unmanned aerial vehicles (UAVs) in three-dimensional space. A cooperative guidance law based on the classic missile-type parallel-approach method is designed for the multi-UAV formation control problem. Additionally, formation transformation strategies for multi-UAV autonomous assembly, disbandment, and special circumstances are formed, effective for managing and controlling the formation. When formulating the management strategy for formation establishment, its process is divided into three steps: (i) selecting and

APA, Harvard, Vancouver, ISO, and other styles

29

Zhang, Jialong, Jianguo Yan, Pu Zhang, Xiaoqiao Qi, and Maolong Lü. "Study on the High-Speed and Close of the UVA Cooperative Formation Controller Design." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 36, no. 2 (2018): 345–52. http://dx.doi.org/10.1051/jnwpu/20183620345.

Full text

Abstract:

Aiming at the high-speed flight of the UAVs cooperative formation, when a single UAV has occurred, need to exit the formation flight and be close or super close to form of the formation quickly. A fast close cooperative formation controller design method is proposed to make up for low the fighting robustness, and be shortcomings of timeliness poorly and analyze the dynamic characteristic of UAV formation flight. Taking the external factors known into consideration, setting up for the longitude maneuver of nonlinear thrust vector and unsteady aerodynamic model, according to the formation veloci

APA, Harvard, Vancouver, ISO, and other styles

30

Tang, Chenchong, Beining Ying, Ruoxuan Gu, and Shengying Yang. "Research on Purely Azimuth Passive Localization Model for UAV Formation Flight." Journal of Physics: Conference Series 2861, no. 1 (2024): 012001. http://dx.doi.org/10.1088/1742-6596/2861/1/012001.

Full text

Abstract:

Abstract The practical applications of unmanned aerial vehicle (UAV) formation passive localization demand high accuracy and anti-interference ability. In this paper, a novel passive localization model based on analytical geometry and improved damped Gauss-Newton optimization method is proposed, which incorporates the improved damped Gauss-Newton algorithm and the error-based iterative algorithm for real-time coordinate correction of formation. Through Matlab simulation experiments, the proposed error-based iterative algorithm can stabilize the flight formation after only 24 iterations, and th

APA, Harvard, Vancouver, ISO, and other styles

31

Büchner, D., J. A. A. Engelbrecht, J. Adams, and C. Redelinghuys. "Towards Automatic Flight Control for Commercial Airliners in Formation Flight." IFAC Proceedings Volumes 47, no. 3 (2014): 12188–94. http://dx.doi.org/10.3182/20140824-6-za-1003.01181.

Full text

APA, Harvard, Vancouver, ISO, and other styles

32

Xu, Linxing, and Yang Li. "Distributed Robust Formation Tracking Control for Quadrotor UAVs with Unknown Parameters and Uncertain Disturbances." Aerospace 10, no. 10 (2023): 845. http://dx.doi.org/10.3390/aerospace10100845.

Full text

Abstract:

In this paper, the distributed formation tracking control problem of quadrotor unmanned aerial vehicles is considered. Adaptive backstepping inherently accommodates model uncertainties and external disturbances, making it a robust choice for the dynamic and unpredictable environments in which unmanned aerial vehicles operate. This paper designs a formation flight control scheme for quadrotor unmanned aerial vehicles based on adaptive backstepping technology. The proposed control scheme is divided into two parts. For the position subsystem, a distributed robust formation tracking control scheme

APA, Harvard, Vancouver, ISO, and other styles

33

İnan, Ahmet Talat, and Mustafa Ceylan. "Aerodynamic Analysis of Fixed-Wing Unmanned Aerial Vehicles Moving in Swarm." Applied Sciences 14, no. 15 (2024): 6463. http://dx.doi.org/10.3390/app14156463.

Full text

Abstract:

This paper presents a close-formation flight of two unmanned aerial vehicles (UAVs) and the aim of the study is to improve the understanding of the vortex effects between fixed-wing UAVs in a swarm using computational fluid dynamics (CFD) tools. To validate the numerical method, results of a variable-density wind tunnel test from the literature were used. This numerical CFD analysis was used to determine the lift coefficient (CL) and the drag coefficient (CD) values for a single UAV at various angles of attack. When examining the aerodynamic impact areas behind the UAV, the longitudinal distan

APA, Harvard, Vancouver, ISO, and other styles

34

Yao, Zheng, Sentang Wu, and Yongming Wen. "Formation Generation for Multiple Unmanned Vehicles Using Multi-Agent Hybrid Social Cognitive Optimization Based on the Internet of Things." Sensors 19, no. 7 (2019): 1600. http://dx.doi.org/10.3390/s19071600.

Full text

Abstract:

Multi-agent hybrid social cognitive optimization (MAHSCO) based on the Internet of Things (IoT) is suggested to solve the problem of the generation of formations of unmanned vehicles. Through the analysis of the unmanned vehicle formation problem, formation principles, formation scale, unmanned vehicle formation safety distance, and formation evaluation indicators are taken into consideration. The application of the IoT enables the optimization of distributed computing. To ensure the reliability of the formation algorithm, the convergence of MAHSCO has been proved. Finally, computer simulation

APA, Harvard, Vancouver, ISO, and other styles

35

Ashokkumar, Chimpalthradi R., George WP York, and Scott F. Gruber. "Nonlinear cooperative UAV maneuvers in pitch plane." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 9 (2016): 1746–55. http://dx.doi.org/10.1177/0954410016656876.

Full text

Abstract:

Flight formations of unmanned aerial vehicles may require coordinated motion in pitch for such tasks as terrain tracking. They maintain a constant altitude over varying terrain elevations and may assist collision avoidance where an altitude change is needed rather than a lateral change. In these maneuvers, controller ability to adjust relative altitude positions (as attractions and repulsions) of the aircraft subject to stability constraints that ends up in a formation shape should be demonstrated. The ascent and descent flight control mode combinations of each unmanned aerial vehicle particip

APA, Harvard, Vancouver, ISO, and other styles

36

Yang, Yuan, Hengnian Li, Yikang Yang, Chongyuan Hou, and Kaijian Zhu. "Close-range leader–follower flight control technology for near-circular low-orbit satellites." Open Astronomy 31, no. 1 (2022): 366–74. http://dx.doi.org/10.1515/astro-2022-0032.

Full text

Abstract:

Abstract Based on the characteristics of near-circular orbits and close-range leader–follower flights, the relative dynamics equations of the eccentricity/inclination ( e/i ) vector method are introduced herein. Additionally, the constraint terms in the design of the leader–follower flight formation are found to satisfy the conditions of the line-of-sight angle and inter-satellite distance. The control box algorithm is proposed under the flying task’s constraints, such as the line-of-sight angle and distance between the satellites according to the e/i vector and Gauss perturbation equations. T

APA, Harvard, Vancouver, ISO, and other styles

37

Kotov, Oleg V., Sergey N. Sinelnikov, Ilya O. Naturalnikov, et al. "Features of flight information perception in shaping the flight concept." Bulletin of the Russian Military Medical Academy 23, no. 4 (2021): 171–78. http://dx.doi.org/10.17816/brmma60341.

Full text

Abstract:

This study determines the peculiarities of perception of aerobatic information in shaping the horizontal flight concept for operators who do not have experience in simulator training. The skill formation assessment in 10 flights was conducted using time indicators and generalized piloting error calculation based on the task. The program of activity concept shaping is developed using complex sensorimotor reactions at the 3rd stage of flight to increase the attention reserves of operators. The distribution of attention was analyzed when recording the coordinates of eye fixation in the designated

APA, Harvard, Vancouver, ISO, and other styles

38

Zhang, Jialong, Bing Xiao, Maolong Lv, and Qiang Zhang. "Design and flight-stability analysis of a closed fixed-wing unmanned aerial vehicle formation controller." Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 233, no. 8 (2018): 1045–54. http://dx.doi.org/10.1177/0959651818821448.

Full text

Abstract:

This article addresses a flight-stability problem for the multiple unmanned aerial vehicles cooperative formation flight in the process of the closed and high-speed flight. The main objective is to design a cooperative formation controller with known external factors, and this controller can keep the consensus of attitude and position and reduce the communication delay between any two unmanned aerial vehicles and increase unmanned aerial vehicles formation cruise time under the known external factors. Known external factors are taken into consideration, and longitude maneuvers using nonlinear

APA, Harvard, Vancouver, ISO, and other styles

39

Brodecki, Marcin, and Kamesh Subbarao. "Autonomous Formation Flight Control System Using In-Flight Sweet-Spot Estimation." Journal of Guidance, Control, and Dynamics 38, no. 6 (2015): 1083–96. http://dx.doi.org/10.2514/1.g000220.

Full text

APA, Harvard, Vancouver, ISO, and other styles

40

Kim, Taegyun, Seungkeun Kim, and Jinyoung Suk. "Formation Flight Simulation and Flight Test of Multiple Ducted-fan UAV." Journal of Institute of Control, Robotics and Systems 25, no. 5 (2019): 398–406. http://dx.doi.org/10.5302/j.icros.2019.19.0047.

Full text

APA, Harvard, Vancouver, ISO, and other styles

41

Ning, S. Andrew, Tristan C. Flanzer, and Ilan M. Kroo. "Aerodynamic Performance of Extended Formation Flight." Journal of Aircraft 48, no. 3 (2011): 855–65. http://dx.doi.org/10.2514/1.c031046.

Full text

APA, Harvard, Vancouver, ISO, and other styles

42

Xu, Jia, S. Andrew Ning, Geoffrey Bower, and Ilan Kroo. "Aircraft Route Optimization for Formation Flight." Journal of Aircraft 51, no. 2 (2014): 490–501. http://dx.doi.org/10.2514/1.c032154.

Full text

APA, Harvard, Vancouver, ISO, and other styles

43

Ning, S. Andrew, Ilan Kroo, Michael J. Aftosmis, Marian Nemec, and James E. Kless. "Extended Formation Flight at Transonic Speeds." Journal of Aircraft 51, no. 5 (2014): 1501–10. http://dx.doi.org/10.2514/1.c032385.

Full text

APA, Harvard, Vancouver, ISO, and other styles

44

Antczak, Adam, Marcin Chmielewski, and Krzysztof Sibilski. "Formation Flight Planning at an Airline." International Review of Aerospace Engineering (IREASE) 14, no. 6 (2021): 309. http://dx.doi.org/10.15866/irease.v14i6.20988.

Full text

APA, Harvard, Vancouver, ISO, and other styles

45

Hemati, Maziar S., Jeff D. Eldredge, and Jason L. Speyer. "Wake Sensing for Aircraft Formation Flight." Journal of Guidance, Control, and Dynamics 37, no. 2 (2014): 513–24. http://dx.doi.org/10.2514/1.61114.

Full text

APA, Harvard, Vancouver, ISO, and other styles

46

Kless, James E., Michael J. Aftosmis, S. Andrew Ning, and Marian Nemec. "Inviscid Analysis of Extended-Formation Flight." AIAA Journal 51, no. 7 (2013): 1703–15. http://dx.doi.org/10.2514/1.j052224.

Full text

APA, Harvard, Vancouver, ISO, and other styles

47

Kong, Edmund M. C., Daniel W. Kwon, Samuel A. Schweighart, Laila M. Elias, Raymond J. Sedwick, and David W. Miller. "Electromagnetic Formation Flight for Multisatellite Arrays." Journal of Spacecraft and Rockets 41, no. 4 (2004): 659–66. http://dx.doi.org/10.2514/1.2172.

Full text

APA, Harvard, Vancouver, ISO, and other styles

48

Song, Eun-Jung. "Decentralized Filters for the Formation Flight." International Journal of Aeronautical and Space Sciences 3, no. 1 (2002): 19–29. http://dx.doi.org/10.5139/ijass.2002.3.1.019.

Full text

APA, Harvard, Vancouver, ISO, and other styles

49

Mikkola, Seppo, and Claudiu-Lucian Prioroc. "Quasi-satellite dynamics in formation flight." Monthly Notices of the Royal Astronomical Society 457, no. 2 (2016): 1137–44. http://dx.doi.org/10.1093/mnras/stw007.

Full text

APA, Harvard, Vancouver, ISO, and other styles

50

Guelman, Mauricio, Klaus Schilling, and Danna Linn Barnett. "Formation flight line of sight guidance." Acta Astronautica 71 (February 2012): 163–69. http://dx.doi.org/10.1016/j.actaastro.2011.08.004.

Full text

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!