المؤلفون: Giovanni Mengali, Marco Bassetto, Alessandro A. Quarta

المصدر: Aerospace, Vol 11, Iss 6, p 427 (2024)

مصطلحات موضوعية: photonic solar sail, comet interceptor mission, heliocentric nodal flyby, long-period comet, spacecraft trajectory design, preliminary mission analysis, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://www.mdpi.com/2226-4310/11/6/427Test; https://doaj.org/toc/2226-4310Test

الوصول الحر: https://doaj.org/article/981130f5ebf743eebb0e9c9f38493ed1Test

المؤلفون: Zichen Fan, Mingying Huo, Song Xu, Jun Zhao, Naiming Qi

المصدر: IEEE Access, Vol 8, Pp 30918-30927 (2020)

مصطلحات موضوعية: Bezier shape-based method, close-range satellites formation, collision-avoidance, low-thrust trajectory approximation, preliminary mission analysis, Electrical engineering. Electronics. Nuclear engineering, TK1-9971

وصف الملف: electronic resource

العلاقة: https://ieeexplore.ieee.org/document/8952712Test/; https://doaj.org/toc/2169-3536Test

الوصول الحر: https://doaj.org/article/9dc6e02785984fca88a2d0a436f0f179Test

المؤلفون: Quarta A, Mengali G, Caruso A

المساهمون: Quarta, A, Mengali, G, Caruso, A

مصطلحات موضوعية: Circumferential propulsive acceleration, rectilinear ellipse, optimal transfer, preliminary mission analysis, quasi-stationary condition

وصف الملف: ELETTRONICO

العلاقة: info:eu-repo/semantics/altIdentifier/wos/WOS:000879889400003; volume:3; issue:1; firstpage:31; lastpage:43; numberofpages:13; journal:ASTRODYNAMICS; http://hdl.handle.net/11568/1011105Test; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-85081731720; https://link.springer.com/article/10.1007/s42064-018-0034-9Test

الإتاحة: https://doi.org/10.1007/s42064-018-0034-9Test
http://hdl.handle.net/11568/1011105Test

المؤلفون: Andrea Caruso, Alessandro A. Quarta, Giovanni Mengali

المصدر: Astrodynamics. 3:31-43

مصطلحات موضوعية: Inertial frame of reference, Aerospace Engineering, quasi-stationary condition, Thrust, 02 engineering and technology, Propulsion, Ellipse, 01 natural sciences, Acceleration, 0203 mechanical engineering, rectilinear ellipse, 0103 physical sciences, Circumferential propulsive acceleration, preliminary mission analysis, Aerospace engineering, 010303 astronomy & astrophysics, Physics, 020301 aerospace & aeronautics, Spacecraft, business.industry, Astronomy and Astrophysics, Parking orbit, optimal transfer, Circumferential propulsive acceleration, rectilinear ellipse, optimal transfer, preliminary mission analysis, quasi-stationary condition, Space and Planetary Science, Physics::Space Physics, Orbit (dynamics), Astrophysics::Earth and Planetary Astrophysics, business

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e111021c1e2c4770d731aad2888d526cTest
https://doi.org/10.1007/s42064-018-0034-9Test

المؤلفون: Fan Zichen, Jun Zhao, Mingying Huo, Song Xu, Naiming Qi

المصدر: IEEE Access, Vol 8, Pp 30918-30927 (2020)

مصطلحات موضوعية: General Computer Science, Computer science, 020209 energy, Computation, Bézier curve, 02 engineering and technology, Space exploration, 0202 electrical engineering, electronic engineering, information engineering, 0601 history and archaeology, General Materials Science, preliminary mission analysis, Fourier series, close-range satellites formation, 060102 archaeology, low-thrust trajectory approximation, General Engineering, Control reconfiguration, 06 humanities and the arts, Trajectory optimization, Solver, Gauss pseudospectral method, collision-avoidance, Bezier shape-based method, lcsh:Electrical engineering. Electronics. Nuclear engineering, Algorithm, lcsh:TK1-9971

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3ca5180aca52e0dfd5b3c3ea6e4bb7c4Test
https://ieeexplore.ieee.org/document/8952712Test/