Works matching DE "ORBITAL transfer (Space flight)"
Results: 152
Orbital transfer vehicle (OTV) system sizing study for manned GEO satellite servicing.
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- Aeronautical Journal, 2016, v. 120, n. 1226, p. 573, doi. 10.1017/aer.2016.3
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Rapid Orbit-to-Orbit Transfer to Asteroid 4660 Nereus Using Solar Electric Propulsion.
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- Universe (2218-1997), 2023, v. 9, n. 11, p. 459, doi. 10.3390/universe9110459
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Solar Sail Trajectories to Earth's Trojan Asteroids.
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- Universe (2218-1997), 2023, v. 9, n. 4, p. 186, doi. 10.3390/universe9040186
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Trajectory Analysis and Optimization of Hesperides Mission.
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- Universe (2218-1997), 2022, v. 8, n. 7, p. N.PAG, doi. 10.3390/universe8070364
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Simulated annealing for solving near-optimal low-thrust orbit transfer.
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- Engineering Optimization, 2005, v. 37, n. 2, p. 201, doi. 10.1080/03052152150512331314533
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Ant Colony Optimization-based Design of Multiple-target Active Debris Removal Mission.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2018, v. 61, n. 5, p. 201, doi. 10.2322/tjsass.61.201
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Earth Escape from a Sun-Earth Halo Orbit using Unstable Manifold and Lunar Swingbys.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 5, p. 269, doi. 10.2322/tjsass.59.269
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Technical Approaches for Improving Accuracy of Initial Orbit Determination in Injection Phase of Earth-Moon Transfer Trajectory.
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- Telecommunication Engineering, 2014, v. 54, n. 6, p. 719, doi. 10.3969/j.issn.1001-893x.2014.06.005
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ON THE ORBITAL PERIOD OF THE EXOPLANET WASP-39 b.
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- Information Bulletin on Variable Stars, 2016, n. 6177, p. 1
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NULL CORRELATION BETWEEN THE O'CONNELL EFFECT AND ORBITAL PERIOD CHANGE FOR SW Lac, CN And, AND V502 Oph.
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- Information Bulletin on Variable Stars, 2015, n. 6127, p. 1
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Frequency stability improvements based on automatic adjustment of synchronous power controller parameters.
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- Electrical Engineering, 2022, v. 104, n. 5, p. 3453, doi. 10.1007/s00202-022-01558-9
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On the Hölder Property of Trajectories in a Set of Full Wiener Measure on the Heisenberg Group.
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- Mathematical Notes, 2019, v. 106, n. 1/2, p. 308, doi. 10.1134/S0001434619070356
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Trajectories of bodies in zones of rapidly decaying triple systems.
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- Astronomy Reports, 2014, v. 58, n. 11, p. 849, doi. 10.1134/S1063772914110031
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Mechanics Model-Based Motion Design for a Piggyback Nursing-Care Robot.
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- Machines, 2022, v. 10, n. 6, p. 441, doi. 10.3390/machines10060441
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Closed shutters or revolving doors? Elite career track similarity and elite sector transfers in Denmark.
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- European Journal of Political Research, 2024, v. 63, n. 3, p. 1022, doi. 10.1111/1475-6765.12627
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DESIGNING RENDEZVOUS MISSIONS WITH MINI-MOONS USING GEOMETRIC OPTIMAL CONTROL.
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- Journal of Industrial & Management Optimization, 2014, v. 10, n. 2, p. 477, doi. 10.3934/jimo.2014.10.477
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Planar tool radius compensation for CNC systems based on NURBS interpolation.
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- Mechanics & Industry, 2020, v. 21, n. 1, p. 1, doi. 10.1051/meca/2019044
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A Recognition Method of Basketball's Shooting Trajectory Based On Transfer Learning.
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- Mobile Networks & Applications, 2022, v. 27, n. 3, p. 1271, doi. 10.1007/s11036-022-01949-z
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Psychology and Wikipedia: Measuring Psychology Journals' Impact by Wikipedia Citations.
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- Social Science Computer Review, 2022, v. 40, n. 3, p. 756, doi. 10.1177/0894439321993836
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Permanent magnet Hall thruster development for future Brazilian space missions.
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- Computational & Applied Mathematics, 2016, v. 35, n. 3, p. 711, doi. 10.1007/s40314-015-0286-4
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Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission.
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- Computational & Applied Mathematics, 2016, v. 35, n. 3, p. 865, doi. 10.1007/s40314-015-0290-8
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Application of a genetic algorithm in orbital maneuvers.
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- Computational & Applied Mathematics, 2015, v. 34, n. 2, p. 437, doi. 10.1007/s40314-014-0151-x
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Pareto Frontier for the time-energy cost vector to an Earth-Moon transfer orbit using the patched-conic approximation.
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- Computational & Applied Mathematics, 2015, v. 34, n. 2, p. 461, doi. 10.1007/s40314-014-0154-7
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基于传热增广模型的轨迹优化与防热结构分析.
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- Systems Engineering & Electronics, 2022, v. 44, n. 3, p. 929, doi. 10.12305/j.issn.1001506X.2022.03.25
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Optimization of fire distribution for multiple SGSW based on improved NSGA-III.
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- Systems Engineering & Electronics, 2020, v. 42, n. 9, p. 1995, doi. 10.3969/j.issn.1001-506X.2020.09.15
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Simulating the SMART1 orbiter impact on the Moon’s surface.
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- Doklady Physics, 2008, v. 53, n. 3, p. 152, doi. 10.1134/S1028335808030099
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Thrust Model and Trajectory Design of an Interplanetary CubeSat with a Hybrid Propulsion System.
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- Actuators, 2024, v. 13, n. 10, p. 384, doi. 10.3390/act13100384
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A Sliding Mode Control-Based Guidance Law for a Two-Dimensional Orbit Transfer with Bounded Disturbances.
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- Actuators, 2023, v. 12, n. 12, p. 444, doi. 10.3390/act12120444
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Continuous-Thrust Circular Orbit Phasing Optimization of Deep Space CubeSats.
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- Applied Sciences (2076-3417), 2024, v. 14, n. 16, p. 7059, doi. 10.3390/app14167059
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Solar Sail-Based Mars-Synchronous Displaced Orbits for Remote Sensing Applications.
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- Applied Sciences (2076-3417), 2024, v. 14, n. 12, p. 5001, doi. 10.3390/app14125001
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Optimal Trajectories of Diffractive Sail to Highly Inclined Heliocentric Orbits.
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- Applied Sciences (2076-3417), 2024, v. 14, n. 7, p. 2922, doi. 10.3390/app14072922
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Solar Sail Transfer Trajectory Design for Comet 29P/Schwassmann–Wachmann 1 Rendezvous.
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- Applied Sciences (2076-3417), 2023, v. 13, n. 17, p. 9590, doi. 10.3390/app13179590
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A Single-Launch Deployment Strategy for Lunar Constellations.
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- Applied Sciences (2076-3417), 2023, v. 13, n. 8, p. 5104, doi. 10.3390/app13085104
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Geometric Analysis of Sun-Assisted Lunar Transfer Trajectories in the Planar Bicircular Four-Body Model.
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- Applied Sciences (2076-3417), 2023, v. 13, n. 8, p. 4676, doi. 10.3390/app13084676
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Integrated Design of Moon-to-Earth Transfer Trajectory Considering Re-Entry Constraints.
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- Applied Sciences (2076-3417), 2022, v. 12, n. 17, p. 8716, doi. 10.3390/app12178716
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Optimal On-Orbit Inspection of Satellite Formation.
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- Remote Sensing, 2022, v. 14, n. 20, p. 5192, doi. 10.3390/rs14205192
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Responses of Ecosystem Services to Land Use/Cover Changes in Rapidly Urbanizing Areas: A Case Study of the Shandong Peninsula Urban Agglomeration.
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- Sustainability (2071-1050), 2024, v. 16, n. 14, p. 6100, doi. 10.3390/su16146100
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Modelization of Low-Cost Maneuvers for an Areostationary Preliminary Mission Design.
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- Mathematical & Computational Applications, 2023, v. 28, n. 6, p. 105, doi. 10.3390/mca28060105
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Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/1364834
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An optimal deployment strategy for multi-plane satellite constellation using a generalized non-planar maneuver.
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- Astrophysics & Space Science, 2024, v. 369, n. 3, p. 1, doi. 10.1007/s10509-024-04288-5
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Optimization of Earth-Mars transfer trajectories with launch constraints.
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- Astrophysics & Space Science, 2022, v. 367, n. 1, p. 1, doi. 10.1007/s10509-021-04025-2
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Low thrust Earth–Moon transfer trajectories via lunar capture set.
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- Astrophysics & Space Science, 2019, v. 364, n. 12, p. 1, doi. 10.1007/s10509-019-3708-8
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Dry mass optimization for the impulsive transfer trajectory of a near-Earth asteroid sample return mission.
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- Astrophysics & Space Science, 2019, v. 364, n. 12, p. 1, doi. 10.1007/s10509-019-3703-0
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Families of Earth–Moon trajectories with applications to transfers towards Sun–Earth libration point orbits.
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- Astrophysics & Space Science, 2019, v. 364, n. 3, p. N.PAG, doi. 10.1007/s10509-019-3532-1
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Parallelly generating halo orbit and its transfer trajectory in the full ephemeris model.
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- Astrophysics & Space Science, 2019, v. 364, n. 1, p. 1, doi. 10.1007/s10509-019-3497-0
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A new probability-one homotopy method for solving minimum-time low-thrust orbital transfer problems.
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- Astrophysics & Space Science, 2018, v. 363, n. 9, p. 1, doi. 10.1007/s10509-018-3420-0
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Design and analysis of Weak Stability Boundary trajectories to Moon.
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- Astrophysics & Space Science, 2018, v. 363, n. 8, p. 1, doi. 10.1007/s10509-018-3378-y
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Determination of the optimal conditions for inclination maneuvers using a Swing-by.
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- Astrophysics & Space Science, 2018, v. 363, n. 5, p. 1, doi. 10.1007/s10509-018-3308-z
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Halo orbit transfer trajectory design using invariant manifold in the Sun-Earth system accounting radiation pressure and oblateness.
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- Astrophysics & Space Science, 2018, v. 363, n. 1, p. 1, doi. 10.1007/s10509-017-3235-4
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Analysis of direct transfer trajectories from LL2 halo orbits to LLOs.
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- Astrophysics & Space Science, 2017, v. 362, n. 9, p. 1, doi. 10.1007/s10509-017-3124-x
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