{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,9,2]],"date-time":"2026-09-02T01:58:24Z","timestamp":1788314304409,"version":"build-2803163510"},"reference-count":26,"publisher":"MDPI AG","issue":"2","license":[{"start":{"date-parts":[[2024,1,19]],"date-time":"2024-01-19T00:00:00Z","timestamp":1705622400000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["Sensors"],"abstract":"<jats:p>Strategy selection is critical for constellation deployment missions, both in terms of energy consumption and time cost. The different effects of impulse thrust and continuous thrust on orbit elements lead to a different choice of strategy. With impulse thrust, constellation types are differentiated according to high and medium-low inclinations. Constellations with high inclination are deployed using a strategy that controls the inclination. Constellations with medium-low inclination are deployed using a strategy that controls the semi-long axis. With continuous thrust, constellations are classified according to high, medium, and low inclination. High inclination constellations are deployed with a strategy of controlling inclination. Medium inclination constellations are deployed with a strategy that controls the semi-long axis. Low inclination constellations are deployed with a strategy of directly applying continuous thrust.<\/jats:p>","DOI":"10.3390\/s24020631","type":"journal-article","created":{"date-parts":[[2024,1,19]],"date-time":"2024-01-19T03:33:41Z","timestamp":1705635221000},"page":"631","update-policy":"https:\/\/doi.org\/10.3390\/mdpi_crossmark_policy","source":"Crossref","is-referenced-by-count":3,"title":["Deployment of Constellation with Different Inclinations Using the Nodal Precession and Thrust"],"prefix":"10.3390","volume":"24","author":[{"ORCID":"https:\/\/orcid.org\/0000-0001-6480-0419","authenticated-orcid":false,"given":"Shuailong","family":"Zhao","sequence":"first","affiliation":[{"name":"Graduate School, Space Engineering University, Beijing 101400, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Qinyu","family":"Zhu","sequence":"additional","affiliation":[{"name":"Graduate School, Space Engineering University, Beijing 101400, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Xuefeng","family":"Tao","sequence":"additional","affiliation":[{"name":"Graduate School, Space Engineering University, Beijing 101400, China"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Yasheng","family":"Zhang","sequence":"additional","affiliation":[{"name":"Graduate School, Space Engineering University, Beijing 101400, China"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"1968","published-online":{"date-parts":[[2024,1,19]]},"reference":[{"key":"ref_1","doi-asserted-by":"crossref","unstructured":"Wang, K., and El-Mowafy, A. 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GALILEO Positioning Technology Signals and Communication Technology, Springer.","DOI":"10.1007\/978-94-007-1830-2"},{"key":"ref_5","doi-asserted-by":"crossref","first-page":"156778","DOI":"10.1109\/ACCESS.2021.3130295","article-title":"Cost Estimation Model for Mega-Constellation Deployment Missions","volume":"9","author":"Jia","year":"2021","journal-title":"IEEE Access"},{"key":"ref_6","doi-asserted-by":"crossref","first-page":"685","DOI":"10.1016\/j.actaastro.2005.03.065","article-title":"Techniques for deploying elliptically orbiting constellations in along-track formation","volume":"57","author":"Bainum","year":"2005","journal-title":"Acta Astronaut."},{"key":"ref_7","unstructured":"Carlo, M., Di Ricciardi, L., and Vasile, M. (2016). AIAA\/AAS Astrodynamics Specialist Conference, Aerospace Research Central."},{"key":"ref_8","doi-asserted-by":"crossref","first-page":"213","DOI":"10.1016\/j.actaastro.2018.03.054","article-title":"Optimization of satellite constellation deployment strategy considering uncertain areas of interest","volume":"153","author":"Lee","year":"2018","journal-title":"Acta Astronaut."},{"key":"ref_9","unstructured":"Wijnen, M., Correyero Plaza, S., P\u00e9rez Grande, D., de Saavedra, B., and Villegas Prado, D. (2022, January 19\u201323). ATHENA a modular, customizable electrospray thruster for pico-, nano- and micro-satellites. Proceedings of the International Electric Propulsion Conference (IEPC), Cambridge, MA, USA."},{"key":"ref_10","unstructured":"Grimaud, L., Krejci, D., and Seifert, B. (2019, January 15\u201320). The IFM Micro FEEP thruster: A modular design for smallsat propulsion. Proceedings of the International Electric Propulsion Conference (IEPC), Vienna, Austria. Available online: https:\/\/electricrocket.org\/2019\/675.pdf."},{"key":"ref_11","doi-asserted-by":"crossref","first-page":"3367","DOI":"10.1109\/TGRS.2008.2005202","article-title":"Constellation deployment for the FORMOSAT-3\/COSMIC mission","volume":"46","author":"Fong","year":"2008","journal-title":"IEEE Trans. Geosci. Remote Sens."},{"key":"ref_12","unstructured":"King, J.A., and Beidleman, N.J. (1993). Method and Apparatus for Deploying a Satellite Network. (5,199,672), U.S. Patent."},{"key":"ref_13","doi-asserted-by":"crossref","first-page":"65","DOI":"10.1016\/j.actaastro.2015.04.015","article-title":"Launch and deployment of distributed small satellite systems","volume":"114","author":"Crisp","year":"2015","journal-title":"Acta Astronaut."},{"key":"ref_14","doi-asserted-by":"crossref","first-page":"243","DOI":"10.1016\/j.actaastro.2018.06.007","article-title":"CubeSat constellation management using Ionic Liquid Electrospray Propulsion","volume":"151","author":"Krejci","year":"2018","journal-title":"Acta Astronaut."},{"key":"ref_15","doi-asserted-by":"crossref","first-page":"23","DOI":"10.1016\/j.actaastro.2015.12.036","article-title":"Deploying a single-launch nanosatellite constellation to several orbital planes using drag maneuvers","volume":"121","author":"Leppinen","year":"2016","journal-title":"Acta Astronaut."},{"key":"ref_16","doi-asserted-by":"crossref","first-page":"159","DOI":"10.1108\/AEAT-02-2014-0023","article-title":"Fuel efficient control strategy for constellation orbital deployment","volume":"88","author":"Yang","year":"2016","journal-title":"Aircr. Eng. Aerosp. Technol."},{"key":"ref_17","doi-asserted-by":"crossref","first-page":"814","DOI":"10.2514\/1.G004443","article-title":"General perturbation method for satellite constellation deployment using nodal precession","volume":"43","author":"McGrath","year":"2020","journal-title":"J. Guid. Control. Dyn."},{"key":"ref_18","doi-asserted-by":"crossref","first-page":"3281","DOI":"10.1016\/j.asr.2022.09.019","article-title":"Optimization of constellation deployment using on-board propulsion and Earth nodal regression","volume":"70","year":"2022","journal-title":"Adv. Space Res."},{"key":"ref_19","unstructured":"Zhang, Y. (2008). Satellite Constellation Theory and Design, Science Press."},{"key":"ref_20","first-page":"28","article-title":"Current Status and Future Prospects of Hall Electric Propulsion Space Applications","volume":"44","author":"Hang","year":"2023","journal-title":"Propuls. Technol."},{"key":"ref_21","doi-asserted-by":"crossref","first-page":"284","DOI":"10.1016\/j.actaastro.2023.07.047","article-title":"Review of Alternative Propellants in Hall Thrusters","volume":"212","author":"Tirila","year":"2023","journal-title":"Acta Astronaut."},{"key":"ref_22","unstructured":"Vallado, D.A. (2013). Fundamentals of Astrodynamics and Applications, Microcosm Press. [4th ed.]."},{"key":"ref_23","doi-asserted-by":"crossref","first-page":"18","DOI":"10.1007\/s40295-023-00381-z","article-title":"Minimum Cost Perturbed Multi-impulsive Maneuver Methodology to Accomplish an Optimal Deployment Scheduling for a Satellite Constellation","volume":"70","author":"Bakhtiari","year":"2023","journal-title":"J. Astronaut. Sci."},{"key":"ref_24","unstructured":"Ruggiero, A., Pergola, P., Marcuccio, S., and Andrenucci, M. (2011, January 11\u201315). Low-Thrust Maneuvers for the Efficient Correction of Orbital Elements. Proceedings of the 32nd International Electric Propulsion Conference, Wiesbaden, Germany. Available online: https:\/\/api.semanticscholar.org\/CorpusID:29040684."},{"key":"ref_25","doi-asserted-by":"crossref","unstructured":"Conway, B.A. (2010). Spacecraft Trajectory Optimization, Cambridge University Press.","DOI":"10.1017\/CBO9780511778025"},{"key":"ref_26","doi-asserted-by":"crossref","unstructured":"Zhao, S., Tao, X., and Li, Z. (2023). Initial Identification of Thrust and Orbit Elements for Continuous Thrust Spacecraft in Circular Orbit. 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