| Orbital dynamics of high area-to-mass ratio spacecraft with J2 and solar radiation pressure for novel Earth observation and communication services C Colombo, C Lücking, CR McInnes Acta Astronautica 81 (1), 137-150, 2012 | 88 | 2012 |
| A passive satellite deorbiting strategy for medium earth orbit using solar radiation pressure and the J2 effect C Lücking, C Colombo, CR McInnes Acta Astronautica 77, 197-206, 2012 | 70 | 2012 |
| Solar radiation pressure-augmented deorbiting: passive end-of-life disposal from high-altitude orbits C Lücking, C Colombo, CR McInnes Journal of Spacecraft and Rockets 50 (6), 1256-1267, 2013 | 56 | 2013 |
| Electrochromic orbit control for smart-dust devices C Lücking, C Colombo, CR McInnes Journal of Guidance, Control, and Dynamics 35 (5), 1548-1558, 2012 | 44 | 2012 |
| Orbit evolution, maintenance and disposal of SpaceChip swarms through electro-chromic control C Colombo, C Lücking, CR McInnes Acta Astronautica 82 (1), 25-37, 2013 | 43 | 2013 |
| Orbital dynamics of high area-to-mass ratio spacecraft under the influence of J2 and solar radiation pressure C Colombo, C Lücking, C McInnes 62nd International Astronautical Congress, 2011 | 23* | 2011 |
| Assessment of passive and active solar sailing strategies for end of life re-entry C Colombo, TDB De Fer International Astronautical Congress, number IAC-16-A6 4, 2016 | 20 | 2016 |
| Heliotropic dust rings for Earth climate engineering R Bewick, C Lücking, C Colombo, JP Sanchez, CR McInnes Advances in Space Research 51 (7), 1132-1144, 2013 | 18 | 2013 |
| Orbit control of high area-to-mass ratio spacecraft using electrochromic coating C Lucking, C Colombo, CR McInnes 61st International Astronautical Congress 2010, IAC 2010, IAC10-C1. 2.7, 2010 | 17 | 2010 |
| Needs assessment of gossamer structures in communications platform end-of-life disposal M Macdonald, C McInnes, C Lücking, L Visagie, VJ Lappas, S Erb AIAA Guidance, Navigation, and Control (GNC) Conference, 4870, 2013 | 16 | 2013 |
| Tandem-L: Main results of the phase a feasibility study G Krieger, A Moreira, M Zink, I Hajnsek, S Huber, M Villano, ... 2016 IEEE International Geoscience and Remote Sensing Symposium (IGARSS …, 2016 | 15 | 2016 |
| Concept-of-operations disposal analysis of spacecraft by gossamer structure M Macdonald, C McInnes, C Bewick, L Visagie, V Lappas, S Erb Journal of Spacecraft and Rockets 52 (2), 517-525, 2015 | 15 | 2015 |
| A passive high altitude deorbiting strategy C Lucking, C Colombo, C McInnes 25th Annual IAA/USU Conference on Small satellites, 2011 | 13 | 2011 |
| Solar radiation pressure augmented deorbiting from high altitude sun-synchronous orbits C Lucking, C Colombo, C McInnes 4S Symposium 2012, Small Satellites Systems and Services, 2012 | 8 | 2012 |
| StrathSat-R: Deploying inflatable CubeSat structures in micro gravity R Clark, T Sinn, C Lucking, N Donaldson, RH Brown, T Parry 63rd International Astronautical Congress, 2012 | 7 | 2012 |
| Collision probability of satellite re-entry with high areato-mass ratio C Lücking, C Colombo, CR McInnes, HG Lewis 9th IAA Symposium on Small Satellites, 08-12, 2013 | 5 | 2013 |
| Geo-engineering using dust grains in heliotropic elliptical orbits R Bewick, C Lucking, C Colombo, JPS Cuartielles, C McInnes 62nd International Astronautical Congress 2011, 2011 | 5 | 2011 |
| Industry Processes for Space Debris Mitigation in Early Mission Definition for LEO Satellites: Current State and Room for Improvement C Bewick, JC Meyer, M Lau, M Peukert 7th ECSD 672, 2017 | 4 | 2017 |
| Mission and system design of a 3U CubeSat for passive GTO to LEO transfer C Lucking, C Colombo, C McInnes 63rd International Astronautical Congress, 2012 | 4 | 2012 |
| Micro-to-macro: astrodynamics at extremes of length-scale C McInnes, M Ceriotti, C Colombo, JPS Cuartielles, R Bewick, J Heiligers, ... Acta Futura 4, 81-97, 2011 | 4 | 2011 |
Colin McInnesJames Watt Chair, Professor of Engineering Science, University of Glasgowglasgow.ac.uk üzerinde doğrulanmış e-posta adresine sahip