Works matching DE "ORBITAL transfer (Space flight)"
Results: 151
On optimal three-impulse Earth–Moon transfers in a four-body model.
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- Celestial Mechanics & Dynamical Astronomy, 2024, v. 136, n. 3, p. 1, doi. 10.1007/s10569-024-10193-4
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Exploring more solutions for low-energy transfers to lunar distant retrograde orbits.
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- Celestial Mechanics & Dynamical Astronomy, 2022, v. 134, n. 1, p. 1, doi. 10.1007/s10569-021-10056-2
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Low-fuel transfers from Mars to quasi-satellite orbits around Phobos exploiting manifolds of tori.
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- Celestial Mechanics & Dynamical Astronomy, 2021, v. 133, n. 5, p. 1, doi. 10.1007/s10569-021-10017-9
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Linking low- to high-energy dynamics of invariant manifolds, transit orbits, and singular collision orbits in the planar circular restricted three-body problem.
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- Celestial Mechanics & Dynamical Astronomy, 2019, v. 131, n. 11, p. N.PAG, doi. 10.1007/s10569-019-9934-0
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Dynamical lifetime survey of geostationary transfer orbits.
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- Celestial Mechanics & Dynamical Astronomy, 2018, v. 130, n. 11, p. 1, doi. 10.1007/s10569-018-9865-1
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Energy preserving low-thrust guidance for orbit transfers in KS variables.
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- Celestial Mechanics & Dynamical Astronomy, 2016, v. 125, n. 1, p. 107, doi. 10.1007/s10569-016-9677-0
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A Hamiltonian approach to the planar optimization of mid-course corrections.
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- Celestial Mechanics & Dynamical Astronomy, 2016, v. 124, n. 4, p. 367, doi. 10.1007/s10569-015-9666-8
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Two-impulse transfer between coplanar elliptic orbits using along-track thrust.
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- Celestial Mechanics & Dynamical Astronomy, 2015, v. 121, n. 3, p. 261, doi. 10.1007/s10569-014-9598-8
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Revisiting Lambert's problem.
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- Celestial Mechanics & Dynamical Astronomy, 2015, v. 121, n. 1, p. 1, doi. 10.1007/s10569-014-9587-y
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A novel algorithm for generating libration point orbits about the collinear points.
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- Celestial Mechanics & Dynamical Astronomy, 2014, v. 120, n. 1, p. 57, doi. 10.1007/s10569-014-9560-9
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Near distance approximation in astrodynamical applications of Lambert's theorem.
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- Celestial Mechanics & Dynamical Astronomy, 2014, v. 118, n. 1, p. 49, doi. 10.1007/s10569-013-9524-5
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A study of low-energy transfer orbits to the Moon: towards an operational optimization technique.
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- Celestial Mechanics & Dynamical Astronomy, 2013, v. 115, n. 3, p. 215, doi. 10.1007/s10569-012-9458-3
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Comparison of low-energy lunar transfer trajectories to invariant manifolds.
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- Celestial Mechanics & Dynamical Astronomy, 2013, v. 115, n. 3, p. 311, doi. 10.1007/s10569-012-9466-3
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Spacecraft intercept using minimum control energy and wait time.
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- Celestial Mechanics & Dynamical Astronomy, 2013, v. 115, n. 1, p. 1, doi. 10.1007/s10569-012-9448-5
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Applicability and dynamical characterization of the associated sets of the algorithmic weak stability boundary in the lunar sphere of influence.
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- Celestial Mechanics & Dynamical Astronomy, 2012, v. 113, n. 2, p. 141, doi. 10.1007/s10569-012-9409-z
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Low-energy, low-thrust transfers to the Moon.
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- Celestial Mechanics & Dynamical Astronomy, 2009, v. 105, n. 1-3, p. 61, doi. 10.1007/s10569-009-9220-7
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Non-Keplerian orbits for electric sails.
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- Celestial Mechanics & Dynamical Astronomy, 2009, v. 105, n. 1-3, p. 179, doi. 10.1007/s10569-009-9200-y
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Extension of fast periodic transfer orbits from the Earth–Moon RTBP to the Sun–Earth–Moon Quasi-Bicircular Problem.
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- Celestial Mechanics & Dynamical Astronomy, 2008, v. 101, n. 3, p. 225, doi. 10.1007/s10569-008-9134-9
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On Targeted Control over Trajectories of Dynamical Systems Arising in Models of Complex Networks.
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- Mathematics (2227-7390), 2023, v. 11, n. 9, p. 2206, doi. 10.3390/math11092206
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Active Debris Removal Mission Planning Method Based on Machine Learning.
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- Mathematics (2227-7390), 2023, v. 11, n. 6, p. 1419, doi. 10.3390/math11061419
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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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Analysis of Correction of the Trajectory of Launching a Spacecraft into High Circular Orbits of an Artificial Moon Satellite Using a Two-Impulse Transfer.
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- Cosmic Research, 2024, v. 62, n. 5, p. 519, doi. 10.1134/S0010952524600823
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A Method for Constructing Low-Energy Trajectories for Earth–Moon Transfers.
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- Cosmic Research, 2024, v. 62, n. 5, p. 454, doi. 10.1134/S0010952524600756
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Optimization of the Spacecraft Transfer Maneuver from a Point of the Elliptical Orbit to Another Point of the Same Orbit.
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- Cosmic Research, 2023, v. 61, n. 5, p. 431, doi. 10.1134/S001095252370034X
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A Method for Calculating the Trajectory of a Single-Impulse Flight to a Halo Orbit around the L<sub>2</sub> Libration Point of the Earth–Moon System.
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- Cosmic Research, 2023, v. 61, n. 5, p. 394, doi. 10.1134/S0010952523700387
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Optimization of the Maneuver to Ensure a High Velocity of the Spacecraft Entry into the Atmosphere.
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- Cosmic Research, 2023, v. 61, n. 5, p. 353, doi. 10.1134/S0010952523700417
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Technique of Optimizing Trajectories of Interplanetary Transfers with Gravity Assisted Maneuvers Using Low-Thrust Propulsion.
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- Cosmic Research, 2019, v. 57, n. 5, p. 339, doi. 10.1134/S0010952519050058
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Analysis of the Structure of Families of Locally Optimum Solutions to the Problem of the Interplanetary Transfer of a Spacecraft with a Low-Thrust Engine.
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- Cosmic Research, 2018, v. 56, n. 5, p. 365, doi. 10.1134/S0010952518050076
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Optimization of transfer trajectories to the Apophis asteroid for spacecraft with high and low thrust.
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- Cosmic Research, 2014, v. 52, n. 2, p. 106, doi. 10.1134/S0010952513060026
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Symmetric periodic solutions of the Hill's problem. I.
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- Cosmic Research, 2013, v. 51, n. 4, p. 275, doi. 10.1134/S0010952513040035
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Optimization of low-thrust orbit transfers with constraints.
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- Cosmic Research, 2012, v. 50, n. 5, p. 376, doi. 10.1134/S0010952512040077
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Numerical solutions to exact equations of motion along near-optimal multi-orbit trajectories for a spacecraft in a Newtonian gravitational field.
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- Cosmic Research, 2011, v. 49, n. 5, p. 424, doi. 10.1134/S001095251104006X
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Quasioptimal control with feedback for multiorbit low-thrust transfer between noncoplanar elliptic and circular orbits.
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- Cosmic Research, 2011, v. 49, n. 2, p. 121, doi. 10.1134/S0010952511010060
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Optimization of low-thrust transfers in the three body problem.
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- Cosmic Research, 2008, v. 46, n. 5, p. 413, doi. 10.1134/S0010952508050080
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Specific features of motion of geosynchronous satellites in the neighborhood of unstable stationary points.
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- Cosmic Research, 2008, v. 46, n. 5, p. 425, doi. 10.1134/S0010952508050092
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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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Trajectories Derived from Periodic Orbits around the Lagrangian Point L 1 and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids.
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- Symmetry (20738994), 2022, v. 14, n. 6, p. N.PAG, doi. 10.3390/sym14061132
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Moonlighting missions.
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- Nature, 2007, v. 450, n. 7172, p. 931, doi. 10.1038/450931a
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- Article
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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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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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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Lifetime Estimation of the Upper Stage of GSAT-14 in Geostationary Transfer Orbit.
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- ISRN Otolaryngology, 2014, p. 1, doi. 10.1155/2014/864953
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An Envelope Algorithm for Single Nanoparticle Collision Electrochemistry<sup>†</sup>.
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- Chinese Journal of Chemistry, 2021, v. 39, n. 7, p. 1936, doi. 10.1002/cjoc.202100079
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Low-Thrust Transfers to Southern L2 Near-Rectilinear Halo Orbits Facilitated by Invariant Manifolds.
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- Journal of Optimization Theory & Applications, 2021, v. 191, n. 2/3, p. 517, doi. 10.1007/s10957-021-01898-9
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Low-Thrust Transfer Design of Low-Observable Geostationary Earth Orbit Satellite.
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- International Journal of Aerospace Engineering, 2015, p. 1, doi. 10.1155/2015/439815
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Solving Coplanar Power-Limited Orbit Transfer Problem by Primer Vector Approximation Method.
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- International Journal of Aerospace Engineering, 2012, p. 1, doi. 10.1155/2012/480320
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Improvement Algorithm of Initial Iterative Value Selecting for Lambert Problem.
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- International Journal of Simulation: Systems, Science & Technology, 2015, v. 16, n. 2B, p. 17.1, doi. 10.5013/IJSSST.a.16.2B.17
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