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Heliocentric solar sail orbit transfers with locally optimal control laws

Macdonald, M. and McInnes, C.R. and Dachwald, B. (2007) Heliocentric solar sail orbit transfers with locally optimal control laws. Journal of Spacecraft and Rockets, 44 (1). pp. 273-276. ISSN 0022-4650

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    Abstract

    Solar sailing is increasingly being considered by space agencies for future science missions. With the absence of reaction mass from the primary propulsion system arises the potential for new high-energy mission concepts in the mid to far term, such as a Solar Polar Orbiter or an Interstellar Heliopause Probe [1,2]. One of the most time consuming tasks of mission analysis is trajectory generation and optimization. Optimal trajectory generation is a complex field and many schemes exist; however, these are typically characterized as being computationally intensive systems requiring a good degree of engineering judgment [3-6].

    Item type: Article
    ID code: 6621
    Keywords: space flight, solar sails, orbits, gravity, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics
    Subjects: Technology > Mechanical engineering and machinery
    Technology > Motor vehicles. Aeronautics. Astronautics
    Department: Faculty of Engineering > Mechanical and Aerospace Engineering
    Related URLs:
    Depositing user: Strathprints Administrator
    Date Deposited: 14 Aug 2008
    Last modified: 04 Oct 2012 12:20
    URI: http://strathprints.strath.ac.uk/id/eprint/6621

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