Heliocentric solar sail orbit transfers with locally optimal control laws
Dachwald, Bernd and Macdonald, M. and McInnes, Colin (2007) Heliocentric solar sail orbit transfers with locally optimal control laws. Journal of Spacecraft and Rockets, 44 (1). pp. 273-276. ISSN 0022-4650 (http://dx.doi.org/10.2514/1.17297)
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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].
ORCID iDs
Dachwald, Bernd, Macdonald, M. ORCID: https://orcid.org/0000-0003-4499-4281 and McInnes, Colin;-
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Item type: Article ID code: 6621 Dates: DateEvent2007PublishedSubjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Strathprints Administrator Date deposited: 14 Aug 2008 Last modified: 11 Nov 2024 08:51 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/6621