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Relevant bibliographies by topics / Flight path correction

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Academic literature on the topic 'Flight path correction'

Author: Grafiati

Published: 4 June 2025

Last updated: 1 August 2025

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Journal articles on the topic "Flight path correction"

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Atygayev, Talgat, Victor Ivel, and Yulia Gerasimova. "Development of a hardware and software model of a rocket motion correction system." Eastern-European Journal of Enterprise Technologies 3, no. 3 (111) (2021): 15–23. http://dx.doi.org/10.15587/1729-4061.2021.228146.

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The paper deals with the development of a motion correction system for an unguided rocket of a certain class. The existing method for calculating the rocket flight range based on the dependence of flight path on the initial rocket pitch angle and average parameters of disturbing effects does not provide the required accuracy of the specified flight range. This is mainly due to uncontrolled range wind deviations in the flight area. At the same time, conducting test rocket launches to identify dispersion characteristics and improve the target accuracy leads to significant material costs. Therefo

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Talgat, Atygayev, Ivel Victor, and Gerasimova Yulia. "Development of a hardware and software model of a rocket motion correction system." Eastern-European Journal of Enterprise Technologies 3, no. 3 (111) (2021): 15–23. https://doi.org/10.15587/1729-4061.2021.228146.

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The paper deals with the development of a motion correction system for an unguided rocket of a certain class. The existing method for calculating the rocket flight range based on the dependence of flight path on the initial rocket pitch angle and average parameters of disturbing effects does not provide the required accuracy of the specified flight range. This is mainly due to uncontrolled range wind deviations in the flight area. At the same time, conducting test rocket launches to identify dispersion characteristics and improve the target accuracy leads to significant material costs. Therefo

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Mandić, S. "Dispersion reduction of artillery rockets guided by flight path steering method." Aeronautical Journal 120, no. 1225 (2016): 435–56. http://dx.doi.org/10.1017/aer.2016.4.

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ABSTRACTArtillery rockets are sensitive to disturbances (total impulse variation, wind, thrust misalignment, etc.). As the range of ground-to-ground rockets increases, the accuracy of free flight rockets decreases. Requirements for the increase of the range and minimisation of the impact point dispersions can be solved by adding guidance and control systems to rockets. Based on the differences between the measured flight parameters and the calculated parameters for the nominal trajectory, the flight path angle correction algorithm is obtained by adding the correction to the nominal value. The

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Gao, Jianfeng, Yu Zheng, Kai Ni, Qiliang Mei, Bin Hao, and Long Zheng. "Fast Path Planning for Firefighting UAV Based on A-Star algorithm." Journal of Physics: Conference Series 2029, no. 1 (2021): 012103. http://dx.doi.org/10.1088/1742-6596/2029/1/012103.

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Abstract When the long distance oil-gas pipeline accident occurs, the fire UAV can give priority to the place where the accident occurs. Emergency investigation and fire rescue, greatly reduces the harm of the accident. However, due to the limitation of the UAV navigation system, the UAV will accumulate the positioning errors over time in the flight process. If the positioning errors can not be corrected in time, it will make the UAV unable to reach the intended destination, thus leading to the failure of the rescue mission. In view of this phenomenon, we propose a UAV path planning scheme con

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Li, Zhao, Weihao Ma, and Haixiang Pang. "Multi-Objective Path Optimization Method for Maritime UAVs Equipped with Inertial Navigation Systems." Journal of Marine Science and Engineering 13, no. 5 (2025): 870. https://doi.org/10.3390/jmse13050870.

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Maritime unmanned aerial vehicles (UAVs) equipped with inertial navigation systems (INS) are prone to error accumulation, which can lead to excessive positioning errors and hinder their ability to perform long distance missions. To address this issue, this study first constructs a directed graph network for a flight area based on start and end points as well as error correction points. A multi-objective route planning model is then developed for a UAV, aiming to minimize both the flight distance and the number of positioning corrections. Considering the UAV’s turning radius, a trajectory lengt

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Cheng, Ningyi, Zhiqian Liu, and Yuqi Li. "Path Planning Algorithm of Dijkstra-Based Intelligent Aircraft under Multiple Constraints." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 6 (2020): 1284–90. http://dx.doi.org/10.1051/jnwpu/20203861284.

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Aiming at the rapid planning of the optimal flight path of the intelligent aircraft, considering the error constraints and correction probability constraints, a model for intelligent aircraft path planning under multiple constraints is constructed, and a global search algorithm based on Dijkstra algorithm is proposed to solve the model. By calculating the residual error and restricts flight distance, the basic Dijkstra algorithm is improved to make it more adaptable to solve the path planning under multiple constraints. At the same time, simulation experiment is conducted with the optimal goal

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Jordan, James F. "Navigation of Spacecraft on Deep Space Missions." Journal of Navigation 40, no. 1 (1987): 19–29. http://dx.doi.org/10.1017/s0373463300000266.

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Spacecraft which are sent on deep space missions to the planets must be accurately navigated in order to achieve the correct flight path. Navigation analysts use precise measurements and large computational software systems to determine a spacecraft's position throughout the mission and compute the velocity corrections for its guidance through space. When the spacecraft is launched into deep space on its voyage, it is impossible to know with great precision where it is headed. Imperfections in both the launch vehicle's terminal velocity and the uncertainty in the knowledge of the parameters wh

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Wang, Lei, Ming Wei, Tao Yang, and Ping Liu. "Effects of Atmospheric Refraction on an Airborne Weather Radar Detection and Correction Method." Advances in Meteorology 2015 (2015): 1–8. http://dx.doi.org/10.1155/2015/407867.

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This study investigates the effect of atmospheric refraction, affected by temperature, atmospheric pressure, and humidity, on airborne weather radar beam paths. Using three types of typical atmospheric background sounding data, we established a simulation model for an actual transmission path and a fitted correction path of an airborne weather radar beam during airplane take-offs and landings based on initial flight parameters and X-band airborne phased-array weather radar parameters. Errors in an ideal electromagnetic beam propagation path are much greater than those of a fitted path when atm

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Agayev, N. B., Q. H. Orujov, and N. N. Kalbiyev. "Planning the Optimal Reference Flight Path of an Aircraft Using a Terrain Map." Mekhatronika, Avtomatizatsiya, Upravlenie 24, no. 9 (2023): 496–502. http://dx.doi.org/10.17587/mau.24.496-502.

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In connection with the development of aviation technology, the expansion of the functionality of modern aircraft and the complication of the tasks being solved, additional stringent requirements are imposed on the accuracy of air navigation. Along with high accuracy, navigation autonomy is also required. The autonomy of aircraft navigation implies the navigation of an aircraft without the use of active radar facilities. In this article, to calculate the optimal reference flight path of an aircraft in a horizontal plane, the Bellman dynamic programming method is proposed using a digital terrain

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Sabatini, Roberto, Terry Moore, and Chris Hill. "A New Avionics-Based GNSS Integrity Augmentation System: Part 2 – Integrity Flags." Journal of Navigation 66, no. 4 (2013): 501–22. http://dx.doi.org/10.1017/s0373463313000143.

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This paper presents the second part of the research activities carried out to develop a novel Global Navigation Satellite System (GNSS) Avionics-Based Integrity Augmentation (ABIA) system for manned and Unmanned Aerial Vehicle (UAV) applications. The ABIA system's architecture was developed to allow real-time avoidance of safety-critical flight conditions and fast recovery of the required navigation performance in case of GNSS data losses. In more detail, our novel ABIA system addresses all four cornerstones of GNSS integrity augmentation in mission- and safety-critical avionics applications:

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Book chapters on the topic "Flight path correction"

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Ivanytskyi, Maxim, Yuliya Averyanova, Yevheniia Znakovska, and Bohdan Shershen. "Aircraft Flight Path Correction During the Flight Execution Phase Using the Operative Information on Weather Hazards." In Proceedings of the 2nd International Workshop on Advances in Civil Aviation Systems Development. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-60196-5_3.

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Ganser, Alexandra. "Going Nowhere: Oceanic Im/Mobilities in North American Refugee Fiction." In Maritime Mobilities in Anglophone Literature and Culture. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-030-91275-8_11.

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AbstractIn philosophy and theory, the terms flight and territorialization are tightly connected to Gilles Deleuze and Félix Guattari’s A Thousand Plateaus. Through “lines of flight”—unpredictable routes defying spatial control—they conceptualize the breakup of a hegemonic spatial semantics through the mobility of the nomad. These lines make the paths of “deterritorialization,” contravening normative spatial structures (“striated” space) and producing “smooth space” that escapes structuration and control. Postcolonial critics such as Gayatri Spivak have held Deleuzian philosophy accountable for

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"Appendix 6: Flight Path Correction." In A Robot Ping-Pong Player. The MIT Press, 2003. http://dx.doi.org/10.7551/mitpress/5985.003.0017.

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Conference papers on the topic "Flight path correction"

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Yilmaz, Ahmet Nuri, and Melahat Cihan. "Comprehensive Simulation of Rocket Flight Trajectories with Active Canard Control for Descent Path Correction." In IAF Space Transportation Solutions and Innovations Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078373-0115.

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Vemprala, Sai, and Srikanth Saripalli. "Collaborative Uncertainty-aware Navigation for Vision based Multirotor Swarms." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12909.

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In this paper, we present a framework for collaborative uncertainty-aware navigation for swarms of vision based multirotor micro aerial vehicles (MAV). We assume that each MAV in a swarm is equipped with a forward-facing monocular camera, and that the vehicles are capable of using feature data to map the environment and perform vision based localization. Additionally, the vehicles are also capable of computing relative poses between each other in order to improve accuracy of pose estimation. For this scenario, we develop a navigation framework which seeks to improve the reconstructed maps and

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Antony, Thomas, and Michael J. Grant. "Correction: Path Constraint Regularization in Optimal Control Problems using Saturation Functions." In 2018 AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0018.c1.

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Sasongko, R. A., and J. Sembiring. "Development of Flight Guidance System of a Small Unmanned Aerial Vehicle (UAV)." In ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/detc2011-48561.

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This paper presents the development of a guidance system for a small Unmanned Aerial Vehicle (UAV) system which combines a waypoints following and an obstacle avoidance systems so that the UAV has a capability to operate in an environment whose ground condition is not completely known. The waypoints following system works by adopting the VOR-Hold approach, in which a correction command will be produced to reduce the angle difference between the desired path and the line connecting the actual UAV position and the subsequent destination point. An avoidance algorithm is developed and integrated w

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Kim, Jung-Hyun, Kisun Song, Seulki Kim, and Dimitri N. Mavris. "Correction: Data-Driven Approach for Understanding the Impact of Weather on Commercial Flight Path." In AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3191.c1.

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Gryshanova, Iryna. "The Effect of Duct Cross-Sectional Shapes on Metrological Performance of Ultrasonic Flowmeters." In ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37383.

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This paper describes prospects of measuring range extension on transient and laminar flow regimes for ultrasonic time-of-flight flowmeters due to creation measuring ducts with special cross-sectional shapes. The appropriateness of this idea consists that the flow profile correction factor, which considers a difference between averaged fluid velocity along the path of ultrasound propagation and area-averaged fluid velocity is not identical for laminar, transitive and turbulent conditions. Even on the assumption of axially symmetric flows the correction factor changes more than on 25% at transit

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Bouskela, Adrien, and Sergey Shkarayev. "Correction: Glider Dynamics Along Ascending and Descending Helical Flight Paths." In AIAA AVIATION FORUM AND ASCEND 2024. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-3572.c1.

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Manikandaswamy, R., M. J. George, and G. Rajesh. "ATTITUDE ESTIMATION AND PRECISION GUIDANCE OF A SPINNING ARTILLERY SHELL." In 34th International Symposium on Ballistics. Destech Publications, Inc., 2025. https://doi.org/10.12783/ballistics25/37188.

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Guided munitions enable precise targeting and minimal collateral damage. Accurately determining an artillery shell’s orientation in flight allows real-time trajectory adjustments for maximum effectiveness. Spinning enhances stability but complicates attitude estimation due to dynamic disturbances. This research explores cost-effective techniques to estimate the attitude of spinning artillery shells using a magnetometer, accelerometer, GPS, and gyroscope integrated into a Kalman filter framework. The estimated orientation (roll, pitch, yaw) enables real-time trajectory corrections. A guidance a

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Wensky, Tobias, Lutz Winkler, and Jens Friedrichs. "Environmental Influences on Engine Performance Degradation." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-22748.

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Environmental influences have an increasing effect on the performance degradation and durability of modern aircraft engines. The study provides information on environmental effects using in-flight engine data and results of engine overhauls performed at MTU Maintenance. According to these investigations global regions are classified into erosive and anthropogenic polluted areas. Both types of regional effects significantly degrade performance and engine durability. The investigation, which is based upon the in-flight data taken from Engine Trend Monitoring (ETM), provides one approach for the

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Gupta, Rohit, and Ilya V. Kolmanovsky. "Governing Parameter Changes in Nonlinear Parameter-Dependent Optimization Problems." In ASME 2013 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/dscc2013-3845.

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The paper treats a class of parameter-dependent optimization/root finding problems where the minimizer or a real root need to be determined as a function of parameter. Applications of parameter-dependent optimization include spacecraft debris avoidance, adaptive control of Hybrid Electric Vehicles, engine mapping and model predictive control. In these and other problems, the parameter changes can be controlled either directly or indirectly. In this paper, the error analysis of a dynamic predictor-corrector Newton’s type algorithm is presented. Based on this analysis, an approach to govern the

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