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- W2040813406 abstract "J2 perturbation and air drag are derived exactly. The dierential equations are composed of two parts, the inertial motion of the reference spacecraft and the relative motion of the chaser with respect to the reference spacecraft. Some useful properties are uncovered. The inertial motion can be described by six variables, the rst ve variables are independent of the sixth variable, namely the the right ascension of the ascending node; The relative motion are also found to be independent of the right ascension of the ascending node of the reference orbit; The air drag has impact on the inertial motion, and the air drag dierence has impact on the relative motion. After the derivation, four potential application areas are discussed: A1-long-time relative motion prediction; A2-eld of view analysis for relative measurement sensor; A3-impact analysis of the coordinate frame precession on reference spacecraft attitude control; A4-impact analysis of the coordinate frame precession on attitude synchronization mission. These application areas show a good and prospective utility of the dynamics dierential equations in formation ying missions." @default.
- W2040813406 created "2016-06-24" @default.
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- W2040813406 date "2010-08-30" @default.
- W2040813406 modified "2023-09-27" @default.
- W2040813406 title "Differential Equations of Relative Motion under the In uence of J2 Perturbation and Air Drag" @default.
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- W2040813406 doi "https://doi.org/10.2514/6.2010-8758" @default.
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