Details

Autor(en) / Beteiligte

• Zhao, Shuailong
• Zhu, Qinyu
• Tao, Xuefeng
• Zhang, Yasheng

Titel

Deployment of Constellation with Different Inclinations Using the Nodal Precession and Thrust

Ist Teil von

• Sensors (Basel, Switzerland), 2024-01, Vol.24 (2), p.631

Ort / Verlag

Switzerland: MDPI AG

Erscheinungsjahr

2024

Quelle

EZB Electronic Journals Library

Beschreibungen/Notizen

• 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.