Colin R McInnes
Affiliations: | 1991 | University of Glasgow, Glasgow, Scotland, United Kingdom |
Area:
solar sailsWebsite:
https://www.gla.ac.uk/schools/engineering/staff/colinmcinnes/Google:
"Colin R McInnes"Bio:
McInnes, Colin R (1991) Advanced Trajectories for Solar Sail Spacecraft. PhD thesis, University of Glasgow. ... I must thank my two supervisors Prof. John Brown and Dr. John Simmons for ideas, enthusiasm and encouragement.
Parents
Sign in to add mentorJohn C. Brown | grad student | 1991 | University of Glasgow | |
(Advanced Trajectories for Solar Sail Spacecraft) |
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Publications
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Viale A, McInnes C, Bailet G, et al. (2021) Asteroid Deflection by Leveraging Rotational Self-Energy Journal of Spacecraft and Rockets. 58: 813-829 |
Viale A, Bailet G, Ceriotti M, et al. (2021) Excavation of artificial caverns inside asteroids by leveraging rotational self-energy Advances in Space Research. 67: 4142-4157 |
Viale A, Ceriotti M, McInnes CR. (2020) Dynamics of a non-rigid Orbital Siphon at a near-Earth asteroid Journal of Guidance Control and Dynamics, 2020 |
Cao J, Clemente C, McInnes CR, et al. (2020) Solar radiation pressure enabled femtosatellite based Earth remote sensing Ieee Transactions On Aerospace and Electronic Systems. 1-1 |
Vergaaij M, McInnes CR, Ceriotti M. (2020) Economic assessment of high-thrust and solar-sail propulsion for near-Earth asteroid mining Advances in Space Research |
Viale A, Ceriotti M, McInnes C. (2020) Dynamics of an orbital siphon anchored to a rotating ellipsoidal asteroid for resource exploitation Acta Astronautica. 177: 561-576 |
Bonetti F, McInnes C. (2019) Space-enhanced terrestrial solar power for equatorial regions Journal of Spacecraft and Rockets. 56: 33-43 |
Liu J, McInnes CR. (2019) Resonant space tethered system for lunar orbital energy harvesting Acta Astronautica. 156: 23-32 |
Bonetti F, McInnes C. (2019) A continuous latitudinal energy balance model to explore non-uniform climate engineering strategies Climate Dynamics. 52: 5739-5757 |
Arnot CS, McInnes CR, McKay RJ, et al. (2018) Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems Celestial Mechanics and Dynamical Astronomy. 130: 12 |