Two-tangent-impulse flyby of space target from an elliptic initial orbit
The problem of two-tangent-impulse space target flyby is drawn in this paper. Unlike the traditional method, the transfer orbit is divided into two parts, i.e. the phasing orbit and the approaching orbit, considering the temporal and the spatial constraint respectively. The method of the phasing orb...
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| Veröffentlicht in: | Advances in space research 2016-05, Vol.57 (10), p.2177-2186 |
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| creator | Zhu, Zhenglong Yan, Ye |
| description | The problem of two-tangent-impulse space target flyby is drawn in this paper. Unlike the traditional method, the transfer orbit is divided into two parts, i.e. the phasing orbit and the approaching orbit, considering the temporal and the spatial constraint respectively. The method of the phasing orbit and approaching orbit determination is formulated firstly. Then, the attainable target areas from a given position on the initial elliptic orbit, the feasible impulse position for approaching to a given point in space and the optimal approaching orbit to a given point are analyzed. Based on the optimal approaching orbit, the optimal solution for target flyby is provided in the time free case, and a suboptimal solution for the case of time-constrained. Numerical simulations demonstrate the application of the solutions to space target flyby in different scenarios. |
| doi_str_mv | 10.1016/j.asr.2016.02.022 |
| format | Article |
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Unlike the traditional method, the transfer orbit is divided into two parts, i.e. the phasing orbit and the approaching orbit, considering the temporal and the spatial constraint respectively. The method of the phasing orbit and approaching orbit determination is formulated firstly. Then, the attainable target areas from a given position on the initial elliptic orbit, the feasible impulse position for approaching to a given point in space and the optimal approaching orbit to a given point are analyzed. Based on the optimal approaching orbit, the optimal solution for target flyby is provided in the time free case, and a suboptimal solution for the case of time-constrained. 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Unlike the traditional method, the transfer orbit is divided into two parts, i.e. the phasing orbit and the approaching orbit, considering the temporal and the spatial constraint respectively. The method of the phasing orbit and approaching orbit determination is formulated firstly. Then, the attainable target areas from a given position on the initial elliptic orbit, the feasible impulse position for approaching to a given point in space and the optimal approaching orbit to a given point are analyzed. Based on the optimal approaching orbit, the optimal solution for target flyby is provided in the time free case, and a suboptimal solution for the case of time-constrained. Numerical simulations demonstrate the application of the solutions to space target flyby in different scenarios.</description><subject>Approach maneuver</subject><subject>Computer simulation</subject><subject>Flyby missions</subject><subject>Impulses</subject><subject>Mathematical models</subject><subject>Optimal orbit maneuver</subject><subject>Optimization</subject><subject>Orbit determination</subject><subject>Phasing</subject><subject>Phasing maneuver</subject><subject>Space target flyby</subject><subject>Tangent-impulse maneuver</subject><subject>Transfer orbits</subject><issn>0273-1177</issn><issn>1879-1948</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNqFkE9LAzEQxYMoWKsfwFuOXnbNZLubLJ6kqBUKXuo5ZLOTkrL_TFKl397UelYYmGF4v2HeI-QWWA4MqvtdroPPeRpzxlPxMzIDKeoM6oU8JzPGRZEBCHFJrkLYMQZcCDYjq83XmEU9bHGImeunfReQ2u7QHOhoaZi0QRq132Kk1o891QPFrnNTdIa6wUWnOzr6xsVrcmF1gm9--5y8Pz9tlqts_fbyunxcZ2ZRFDErubR1w1ohgbUGoEHNa2mtNBZMiZiWhtetsFZzWVZFJTlWwLXUumgWrS7m5O50d_Ljxx5DVL0LJv2kBxz3QYFkMnkrRfG_VKSAJNQ_UjhJjR9D8GjV5F2v_UEBU8eA1U6lgNUxYMV4Kp6YhxODye6nQ6-CcTgYbJ1HE1U7uj_ob1lUg8Q</recordid><startdate>20160515</startdate><enddate>20160515</enddate><creator>Zhu, Zhenglong</creator><creator>Yan, Ye</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TG</scope><scope>KL.</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20160515</creationdate><title>Two-tangent-impulse flyby of space target from an elliptic initial orbit</title><author>Zhu, Zhenglong ; Yan, Ye</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c433t-528f9b0d7810dc11bea298ff8cf1c5ee0dcc29d7ffa28563682e612a8aa3b4da3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Approach maneuver</topic><topic>Computer simulation</topic><topic>Flyby missions</topic><topic>Impulses</topic><topic>Mathematical models</topic><topic>Optimal orbit maneuver</topic><topic>Optimization</topic><topic>Orbit determination</topic><topic>Phasing</topic><topic>Phasing maneuver</topic><topic>Space target flyby</topic><topic>Tangent-impulse maneuver</topic><topic>Transfer orbits</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhu, Zhenglong</creatorcontrib><creatorcontrib>Yan, Ye</creatorcontrib><collection>CrossRef</collection><collection>Meteorological & Geoastrophysical Abstracts</collection><collection>Meteorological & Geoastrophysical Abstracts - Academic</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Advances in space research</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhu, Zhenglong</au><au>Yan, Ye</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Two-tangent-impulse flyby of space target from an elliptic initial orbit</atitle><jtitle>Advances in space research</jtitle><date>2016-05-15</date><risdate>2016</risdate><volume>57</volume><issue>10</issue><spage>2177</spage><epage>2186</epage><pages>2177-2186</pages><issn>0273-1177</issn><eissn>1879-1948</eissn><abstract>The problem of two-tangent-impulse space target flyby is drawn in this paper. 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| issn | 0273-1177 1879-1948 |
| language | eng |
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| source | Elsevier ScienceDirect Journals |
| subjects | Approach maneuver Computer simulation Flyby missions Impulses Mathematical models Optimal orbit maneuver Optimization Orbit determination Phasing Phasing maneuver Space target flyby Tangent-impulse maneuver Transfer orbits |
| title | Two-tangent-impulse flyby of space target from an elliptic initial orbit |
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