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Research Article

Smart dust option for geomagnetic tail exploration

Alessandro A. Quarta( )Giovanni MengaliLorenzo Niccolai
Department of Civil and Industrial Engineering, University of Pisa, Pisa I-56122, Italy
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Abstract

In-situ measurements are necessary for a long-term analysis of the spatial structure of the geomagnetic tail. This type of mission requires the use of a propellantless propulsion system, such as a classical solar sail, to continuously rotate the design orbit apse line such that it remains parallel to the Sun-Earth direction. To reduce the mission costs, this paper suggests the employment of Sun-pointing smart dusts, which are here investigated in terms of propulsive acceleration level necessary to guarantee a mission’s feasibility. A Sun-pointing smart dust can be thought of as a millimeter-scale solar sail, whose geometric configuration allows it to passively maintain an alignment with the Sun-spacecraft line. The smart dust external surface is coated with an electrochromic reflective film in such a way that it may change, within some limits, its propulsive acceleration magnitude. A suitable control law is necessary for the smart dust to enable an artificial precession of its Earth-centred orbit, similar to what happens in the GeoSail mission. This paper analyzes the required control law using an optimal approach. In particular, the proposed mathematical model provides a set of approximate equations that allow a simple and effective tradeoff analysis between the propulsive requirements, in terms of the smart dust acceleration, and the characteristics of the design orbit.

References

[1]
Kivelson, M. G., Bagenal, F. Planetary mag-netospheres. In: Encyclopedia of the Solar System 3rd edn. Spohn, T., Breuer, D., Johnson, T. V. Eds. Boston: Elsevier, 2014: 137-157.
[2]
Macdonald, M., McInnes, C. R., Alexander, D., Sandman, A. GeoSail: Exploring the magnetosphere using a low-cost solar sail. Acta Astronautica, 2006, 59(8-11): 757-767.
[3]
McInnes, C. R., MacDonald, M., Angelopolous, V., Alexander, D. GEOSAIL: exploring the geomagnetic tail using a small solar sail. Journal of Spacecraft and Rockets, 2001, 38(4): 622-629.
[4]
Falkner, P. Executive summary of the GeoSail study. European Space Agency, Technology Reference Study SCI-A/2006/005/GS, 2007.
[5]
Lappas, V., Mengali, G., Quarta, A. A., Gil-Fernandez, J., Schmidt, T., Wie, B. Practical systems design for an earth-magnetotail-monitoring solar sail mission. Journal of Spacecraft and Rockets, 2009, 46(2): 381-393.
[6]
Wright, J. L. Space Sailing. Philadelphia: Gordon and Breach Science Publishers, 1992: 223.
[7]
Mengali, G., Quarta, A. A., Lappas, V. J. Optimal steering law for the GeoSail mission. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 876-879.
[8]
Colombo, C., McInnes, C. R. Orbital dynamics of “Smart-Dust” devices with solar radiation pressure and drag.Journal of Guidance, Control, and Dynamics, 2011, 34(6): 1613-1631.
[9]
Colombo, C., Lücking, C., McInnes, C. R. Orbital dynamics of high area-to-mass ratio spacecraft with J2 and solar radiation pressure for novel Earth observation and communication services. Acta Astronautica, 2012, 81(1): 137-150.
[10]
Colombo, C., McInnes, C. R. Orbit design for future SpaceChip swarm missions in a planetary atmosphere. Acta Astronautica, 2012, 75: 25-41.
[11]
Colombo, C., Lücking, C., McInnes, C. R. Orbit evolution, maintenance and disposal of SpaceChip swarms through electro-chromic control. ActaAstronautica, 2013, 82(1): 25-37.
[12]
Atchison, J. A., Peck, M. A. A passive, sun-pointing, millimeter-scale solar sail. Acta Astronautica, 2010, 67(1-2): 108-121.
[13]
Niccolai, L., Bassetto, M., Quarta, A. A., Mengali, G. A review of Smart Dust architecture, dynamics, and mission applications. Progress in Aerospace Sciences, 2019, 106: 1-14.
[14]
Lücking, C., Colombo, C., McInnes, C. R. Orbit control of high area-to-mass ratio spacecraft using electrochromic coating. In: Proceedings of the 61st International Astronautical Congress, 2010: 1923-1937.
[15]
Lücking, C., Colombo, C., McInnes, C. R. Electro-chromic orbit control for smart-dust devices. Journal of Guidance, Control, and Dynamics, 2012, 35(5): 1548-1558.
[16]
Manchester, Z., Peck, M., Filo, A. KickSat: A crowd-funded mission to demonstrate the world’s smallest spacecraft. In: Proceedings of the 27th Annual AIAA/USU Conference on Small Satellites, 2013: SSC13-IX-5.
[17]
Fortescue, P., Swinerd, G., Stark, J. Spacecraft Systems Engineering, 4th edn. Chichester: John Wiley & Sons, Ltd, 2011: 93-95.
[18]
Mengali, G., Quarta, A. A. Heliocentric trajectory analysis of sun-pointing smart dust with electrochromic control. Advances in Space Research, 2016, 57(4): 991-1001.
[19]
Quarta, A. A., Mengali, G., Denti, E. Optimal in-orbit repositioning of sun-pointing smart dust. Acta Astronautica, 2019, 154: 278-285.
[20]
Mengali, G., Quarta, A. A., Denti, E. Relative motion of sun-pointing smart dust in circular heliocentric orbits. Journal of Guidance, Control and Dynamics, 2018, 41(4): 1009-1014.
[21]
McInnes, C. R. Solar Sailing: Technology, Dynamics and Mission Applications. London: Springer-Verlag Berlin Heidelberg, 1999: 46-51.
[22]
Mengali, G., Quarta, A. A., Circi, C., Dachwald, B. Rened solar sail force model with mission application. Journal of Guidance, Control, and Dynamics, 2007, 30(2): 512-520.
[23]
Alexander, D., McInnes, C. R., Angelopoulos, V., Sandman, A. W., Macdonald, M. GeoSail: A novel solar sail mission concept for geospace. AIP Conference Proceedings, 2002, 608(1): 305-312.
[24]
Bryson, A. E., Ho, Y. C. Applied Optimal Control. Washington, D. C.: Hemisphere Publishing Corporation. 1975: 71-89.
[25]
Stengel, R. F. Optimal Control and Estimation. New York: Dover Publications. 1994: 222-254.
[26]
Quarta, A. A., Mengali, G., Caruso, A. Optimal circle-to-rectilinear orbit transfer with circumferential thrust. Astrodynamics, 2019, 3(1): 31-43.
[27]
Shampine, L. F., Gordon, M. K. Computer Solution of Ordinary Differential Equations: the Initial Value Pro-blem. New York: W. H. Freeman and Company. 1975.
[28]
Shampine, L. F., Reichelt, M. W. The MATLAB ODE suite. SIAM Journal on Scientific Computing, 1997, 18(1): 1-22.
[29]
Dachwald, B., Seboldt, W., MacDonald, M., Mengali, G., Quarta, A., McInnes, C., Rios-Reyes, L., Scheeres, D., Wie, B., Görlich, M. et al. Potential solar sail degradation effects on trajectory and attitude control. In: Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005: AIAA 2005-6172.
[30]
Dachwald, B., Mengali, G., Quarta, A. A., Macdonald, M. Parametric model and optimal control of solar sails with optical degradation. Journal of Guidance, Control, and Dynamics, 2006, 29(5): 1170-1178.
[31]
Dachwald, B., Macdonald, M., McInnes, C. R., Mengali, G., Quarta, A. A. Impact of optical degradation on solar sail mission performance. Journal of Spacecraft and Rockets, 2007, 44(4): 740-749.
[32]
Mathews, J. H., Fink, K. D. Numerical Methods Using MATLAB, 4th edn. New York: Pearson, 2004: 392-399.
[33]
Prussing, J. E., Conway, B. A. Orbital Mechanics. Oxford: Oxford University Press, 1993: 26-32.
[34]
Aliasi, G., Mengali, G., Quarta, A. A. Artificial Lagrange points for solar sail with electrochromic material panels. Journal of Guidance, Control, and Dynamics, 2013, 36(5): 1544-1550.
Astrodynamics
Pages 217-230
Cite this article:
Quarta AA, Mengali G, Niccolai L. Smart dust option for geomagnetic tail exploration. Astrodynamics, 2019, 3(3): 217-230. https://doi.org/10.1007/s42064-019-0048-3

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Received: 15 December 2018
Accepted: 05 February 2019
Published: 13 August 2019
© Tsinghua University Press 2019
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