Year |
Citation |
Score |
2021 |
Viale A, McInnes C, Bailet G, Ceriotti M. Asteroid Deflection by Leveraging Rotational Self-Energy Journal of Spacecraft and Rockets. 58: 813-829. DOI: 10.2514/1.A34889 |
0.602 |
|
2021 |
Viale A, Bailet G, Ceriotti M, McInnes C. Excavation of artificial caverns inside asteroids by leveraging rotational self-energy Advances in Space Research. 67: 4142-4157. DOI: 10.1016/J.ASR.2021.02.021 |
0.604 |
|
2020 |
Viale A, Ceriotti M, McInnes CR. Dynamics of a non-rigid Orbital Siphon at a near-Earth asteroid Journal of Guidance Control and Dynamics, 2020. DOI: 10.2514/1.G004894 |
0.715 |
|
2020 |
Cao J, Clemente C, McInnes CR, Soraghan JJ. Solar radiation pressure enabled femtosatellite based Earth remote sensing Ieee Transactions On Aerospace and Electronic Systems. 1-1. DOI: 10.1109/Taes.2020.2972242 |
0.463 |
|
2020 |
Vergaaij M, McInnes CR, Ceriotti M. Economic assessment of high-thrust and solar-sail propulsion for near-Earth asteroid mining Advances in Space Research. DOI: 10.1016/J.Asr.2020.06.012 |
0.422 |
|
2020 |
Viale A, Ceriotti M, McInnes C. Dynamics of an orbital siphon anchored to a rotating ellipsoidal asteroid for resource exploitation Acta Astronautica. 177: 561-576. DOI: 10.1016/J.Actaastro.2020.08.001 |
0.699 |
|
2019 |
Bonetti F, McInnes C. Space-enhanced terrestrial solar power for equatorial regions Journal of Spacecraft and Rockets. 56: 33-43. DOI: 10.2514/1.A34032 |
0.414 |
|
2019 |
Liu J, McInnes CR. Resonant space tethered system for lunar orbital energy harvesting Acta Astronautica. 156: 23-32. DOI: 10.1016/J.Actaastro.2018.08.037 |
0.362 |
|
2019 |
Bonetti F, McInnes C. A continuous latitudinal energy balance model to explore non-uniform climate engineering strategies Climate Dynamics. 52: 5739-5757. DOI: 10.1007/S00382-018-4474-Y |
0.34 |
|
2018 |
Arnot CS, McInnes CR, McKay RJ, Macdonald M, Biggs J. 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. PMID 33184531 DOI: 10.1007/S10569-017-9807-3 |
0.461 |
|
2018 |
Viale A, McInnes C, Ceriotti M. Analytical mechanics of asteroid disassembly using the Orbital Siphon effect. Proceedings. Mathematical, Physical, and Engineering Sciences. 474: 20180594. PMID 30602939 DOI: 10.1098/rspa.2018.0594 |
0.68 |
|
2018 |
Bonetti F, McInnes C. Multiple input control strategies for robust and adaptive climate engineering in a low-order 3-box model. Proceedings of the Royal Society a: Mathematical, Physical and Engineering Sciences. 474: 20180447-20180447. PMID 30333711 DOI: 10.1098/Rspa.2018.0447 |
0.319 |
|
2018 |
McInnes CR, Peloni A, Ceriotti M. Osculating Keplerian Elements for Highly Non-Keplerian Orbits Journal of Guidance Control and Dynamics. 41: 2489-2498. DOI: 10.2514/1.G002867 |
0.321 |
|
2018 |
Viale A, Ceriotti M, McInnes CR. Analytical mechanics of asteroid disassembly using the Orbital Siphon effect Proceeding of the Royal Society, Part A. DOI: 10.1098/Rspa.2018.0594 |
0.691 |
|
2018 |
Liu J, McInnes CR. Modulated solar pressure-based surface shape control of paraboloid space reflectors with an off-axis Sun-line Smart Materials and Structures. 27: 35012. DOI: 10.1088/1361-665X/Aaac3A |
0.388 |
|
2018 |
Liu X, McInnes C, Ceriotti M. Strategies to engineer the capture of a member of a binary asteroid pair using the planar parabolic restricted three-body problem Planetary and Space Science. 161: 5-25. DOI: 10.1016/J.Pss.2018.05.018 |
0.375 |
|
2018 |
Tan M, McInnes C, Ceriotti M. Low-energy near Earth asteroid capture using Earth flybys and aerobraking Advances in Space Research. 61: 2099-2115. DOI: 10.1016/J.Asr.2018.01.027 |
0.423 |
|
2018 |
Tan M, McInnes C, Ceriotti M. Capture of small near-Earth asteroids to Earth orbit using aerobraking Acta Astronautica. 152: 185-195. DOI: 10.1016/J.Actaastro.2018.08.007 |
0.466 |
|
2018 |
Salazar FJT, Winter OC, McInnes CR. Collecting solar power by formation flying systems around a geostationary point Computational & Applied Mathematics. 37: 84-95. DOI: 10.1007/S40314-017-0473-6 |
0.478 |
|
2017 |
Zhang J, McInnes CR, Xu M. Reconfiguration of a smart surface using heteroclinic connections. Proceedings. Mathematical, Physical, and Engineering Sciences. 473: 20160614. PMID 28265191 DOI: 10.1098/Rspa.2016.0614 |
0.324 |
|
2017 |
Tan M, McInnes CR, Ceriotti M. Low-energy near-Earth asteroid capture using momentum exchange strategies Journal of Guidance Control and Dynamics. 41: 632-643. DOI: 10.2514/1.G002957 |
0.385 |
|
2017 |
Xu M, McInnes CR. Wavelike Patterns in Precessing Elliptical Rings for Swarming Systems Journal of Guidance Control and Dynamics. 40: 1651-1663. DOI: 10.2514/1.G002476 |
0.388 |
|
2017 |
Xu M, McInnes CR. Closed-loop control of the orbit evolution of ‘smart dust’ swarms Journal of Guidance Control and Dynamics. 40: 1806-1814. DOI: 10.2514/1.G002386 |
0.367 |
|
2017 |
Tan M, McInnes C, Ceriotti M. Direct and indirect capture of near-Earth asteroids in the Earth–Moon system Celestial Mechanics and Dynamical Astronomy. 129: 57-88. DOI: 10.1007/S10569-017-9764-X |
0.42 |
|
2017 |
Salazar FJT, McInnes CR, Winter OC. Periodic orbits for space-based reflectors in the circular restricted three-body problem Celestial Mechanics and Dynamical Astronomy. 128: 95-113. DOI: 10.1007/S10569-016-9739-3 |
0.481 |
|
2016 |
McInnes CR. Near Earth asteroid resource utilisation for large in-orbit reflectors Space Policy. 37: 62-64. DOI: 10.1016/J.Spacepol.2016.07.001 |
0.393 |
|
2016 |
Salazar FJT, McInnes CR, Winter OC. Intervening in Earth's climate system through space-based solar reflectors Advances in Space Research. 58: 17-29. DOI: 10.1016/J.Asr.2016.04.007 |
0.437 |
|
2016 |
McInnes CR. A continuum model for the orbit evolution of self-propelled ‘smart dust’ swarms Celestial Mechanics and Dynamical Astronomy. 1-17. DOI: 10.1007/S10569-016-9707-Y |
0.329 |
|
2015 |
Borggräfe A, Heiligers J, Ceriotti M, McInnes CR. Shape control of slack space reflectors using modulated solar pressure. Proceedings. Mathematical, Physical, and Engineering Sciences / the Royal Society. 471: 20150119. PMID 26345083 DOI: 10.1098/Rspa.2015.0119 |
0.386 |
|
2015 |
Sánchez JP, McInnes CR. Optimal Sunshade Configurations for Space-Based Geoengineering near the Sun-Earth L1 Point. Plos One. 10: e0136648. PMID 26309047 DOI: 10.1371/Journal.Pone.0136648 |
0.429 |
|
2015 |
Verrier PE, Mcinnes CR. Low-energy capture of asteroids onto kolmogorov-arnold-moser tori Journal of Guidance, Control, and Dynamics. 38: 330-334. DOI: 10.2514/1.G000797 |
0.348 |
|
2015 |
Heiligers J, McInnes CR. Engineering notes: Solar sail heliocentric earth-following orbits Journal of Guidance, Control, and Dynamics. 38: 937-944. DOI: 10.2514/1.G000579 |
0.479 |
|
2015 |
Yárnoz DG, Cuartielles JS, McInnes CR. Alternating Orbiter Strategy for Asteroid Exploration Journal of Guidance Control and Dynamics. 38: 280-291. DOI: 10.2514/1.G000562 |
0.463 |
|
2015 |
Borggräfe A, Heiligers J, McInnes CR, Ceriotti M. Attitude dynamics of the classical dumbbell problem with solar radiation pressure Journal of Guidance, Control, and Dynamics. 38: 168-173. DOI: 10.2514/1.G000392 |
0.458 |
|
2015 |
Macdonald M, McInnes C, Bewick C, Visagie L, Lappas V, Erb S. Concept-of-operations disposal analysis of spacecraft by gossamer structure Journal of Spacecraft and Rockets. 52: 517-525. DOI: 10.2514/1.A32919 |
0.365 |
|
2015 |
Mushet G, Mingotti G, Colombo C, Mcinnes C. Self-organising satellite constellation in geostationary earth orbit Ieee Transactions On Aerospace and Electronic Systems. 51: 910-923. DOI: 10.1109/Taes.2014.130690 |
0.391 |
|
2015 |
Zhang J, McInnes CR. Reconfiguring smart structures using approximate heteroclinic connections Smart Materials and Structures. 24: 105034. DOI: 10.1088/0964-1726/24/10/105034 |
0.308 |
|
2015 |
Zhang J, McInnes CR. Reconfiguration of a four-bar mechanism using phase space connections Mechanical Systems and Signal Processing. DOI: 10.1016/J.Ymssp.2016.03.024 |
0.324 |
|
2015 |
Heiligers J, Mingotti G, McInnes CR. Optimal solar sail transfers between halo orbits of different sun-planet systems Advances in Space Research. 55: 1405-1421. DOI: 10.1016/J.Asr.2014.11.033 |
0.453 |
|
2015 |
Heiligers J, Hiddink S, Noomen R, McInnes CR. Solar sail Lyapunov and Halo orbits in the Earth–Moon three-body problem Acta Astronautica. 116: 25-35. DOI: 10.1016/J.Actaastro.2015.05.034 |
0.485 |
|
2015 |
Yárnoz DG, Scheeres DJ, McInnes CR. On the \(a\) and \(g\) families of orbits in the Hill problem with solar radiation pressure and their application to asteroid orbiters Celestial Mechanics and Dynamical Astronomy. 121: 365-384. DOI: 10.1007/S10569-015-9604-9 |
0.387 |
|
2014 |
McInnes CR. Approximate closed-form solution for solar sail spiral trajectories with sail degradation Journal of Guidance, Control, and Dynamics. 37: 2053-2057. DOI: 10.2514/1.G000225 |
0.434 |
|
2014 |
Ceriotti M, Heiligers J, McInnes CR. Trajectory and spacecraft design for a pole-sitter mission Journal of Spacecraft and Rockets. 51: 311-326. DOI: 10.2514/1.A32477 |
0.452 |
|
2014 |
Yarnoz DG, Cuartielles JS, McInnes C. Passive Sorting of Asteroid Material Using Solar Radiation Pressure Journal of Guidance Control and Dynamics. 37: 1223-1235. DOI: 10.2514/1.62412 |
0.381 |
|
2014 |
Verrier P, McInnes C. Periodic orbits for three and four co-orbital bodies Monthly Notices of the Royal Astronomical Society. 442: 3179-3191. DOI: 10.1093/Mnras/Stu1056 |
0.373 |
|
2014 |
Borggräfe A, Heiligers J, Ceriotti M, McInnes CR. Inverse problem for shape control of flexible space reflectors using distributed solar pressure Smart Materials and Structures. 23. DOI: 10.1088/0964-1726/23/7/075026 |
0.323 |
|
2014 |
Ceriotti M, McInnes CR. Design of ballistic three-body trajectories for continuous polar earth observation in the Earth-Moon system Acta Astronautica. 102: 178-189. DOI: 10.1016/J.Actaastro.2014.06.001 |
0.4 |
|
2014 |
Simo J, McInnes CR. Feedback stabilization of displaced periodic orbits: Application to binary asteroids Acta Astronautica. 96: 106-115. DOI: 10.1016/J.Actaastro.2013.11.026 |
0.452 |
|
2014 |
Heiligers J, Ceriotti M, McInnes CR, Biggs JD. Mission analysis and systems design of a near-term and far-term pole-sitter mission Acta Astronautica. 94: 455-469. DOI: 10.1016/J.Actaastro.2012.12.015 |
0.482 |
|
2014 |
Mingotti G, Sánchez JP, McInnes CR. Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun–Earth circular restricted three-body problem Celestial Mechanics and Dynamical Astronomy. 120: 309-336. DOI: 10.1007/S10569-014-9589-9 |
0.461 |
|
2014 |
Heiligers J, McInnes CR. New families of Sun-centered non-Keplerian orbits over cylinders and spheres Celestial Mechanics and Dynamical Astronomy. 120: 163-194. DOI: 10.1007/S10569-014-9570-7 |
0.462 |
|
2013 |
Lücking C, Colombo C, McInnes CR. Solar Radiation Pressure-Augmented Deorbiting: Passive End-of-Life Disposal from High-Altitude Orbits Journal of Spacecraft and Rockets. 50: 1256-1267. DOI: 10.2514/1.A32478 |
0.467 |
|
2013 |
Stolbunov V, Ceriotti M, Colombo C, McInnes CR. Optimal law for inclination change in an atmosphere through solar sailing Journal of Guidance, Control, and Dynamics. 36: 1310-1323. DOI: 10.2514/1.59931 |
0.459 |
|
2013 |
McInnes CR, Colombo C. Wave-like patterns in an elliptical satellite ring Journal of Guidance, Control, and Dynamics. 36: 1767-1771. DOI: 10.2514/1.55956 |
0.355 |
|
2013 |
White C, Colombo C, Scanlon TJ, McInnes CR, Reese JM. Rarefied Gas Effects on the Aerodynamics of High Area-to-Mass Ratio Spacecraft in Orbit Advances in Space Research. 51: 2112-2124. DOI: 10.1016/J.Asr.2013.01.002 |
0.37 |
|
2013 |
Bewick R, Lücking C, Colombo C, Sanchez JP, McInnes CR. Heliotropic dust rings for Earth climate engineering Advances in Space Research. 51: 1132-1144. DOI: 10.1016/J.Asr.2012.10.024 |
0.465 |
|
2013 |
Colombo C, Lücking C, McInnes CR. Orbit evolution, maintenance and disposal of SpaceChip swarms through electro-chromic control Acta Astronautica. 82: 25-37. DOI: 10.1016/J.Actaastro.2012.05.035 |
0.444 |
|
2013 |
Yárnoz DG, Sanchez JP, McInnes CR. Easily retrievable objects among the NEO population Celestial Mechanics and Dynamical Astronomy. 116: 367-388. DOI: 10.1007/S10569-013-9495-6 |
0.402 |
|
2012 |
Johnson L, Young R, Barnes N, Friedman L, Lappas V, McInnes C. Solar Sails: Technology and demonstration status International Journal of Aeronautical and Space Sciences. 13: 421-427. DOI: 10.5139/Ijass.2012.13.4.421 |
0.428 |
|
2012 |
Lücking C, Colombo C, McInnes CR. Electrochromic orbit control for smart-dust devices Journal of Guidance Control and Dynamics. 35: 1548-1558. DOI: 10.2514/1.55488 |
0.458 |
|
2012 |
Bennet DJ, McInnes C. Pattern transition in spacecraft formation flying using bifurcating potential fields Aerospace Science and Technology. 23: 250-262. DOI: 10.1016/J.Ast.2011.07.013 |
0.397 |
|
2012 |
Bewick R, Sanchez JP, McInnes CR. Gravitationally bound geoengineering dust shade at the inner Lagrange point Advances in Space Research. 50: 1405-1410. DOI: 10.1016/J.Asr.2012.07.008 |
0.429 |
|
2012 |
Bewick R, Cuartielles JS, McInnes C. The feasibility of using an L1 positioned dust cloud as a method of space-based geoengineering Advances in Space Research. 49: 1212-1228. DOI: 10.1016/J.Asr.2012.01.010 |
0.403 |
|
2012 |
Sanchez JP, McInnes CR. Synergistic approach of asteroid exploitation and planetary protection Advances in Space Research. 49: 667-685. DOI: 10.1016/J.Asr.2011.11.014 |
0.422 |
|
2012 |
Colombo C, Lücking C, McInnes CR. Orbital dynamics of high area-to-mass ratio spacecraft with J2 and solar radiation pressure for novel Earth observation and communication services Acta Astronautica. 81: 137-150. DOI: 10.1016/J.Actaastro.2012.07.009 |
0.48 |
|
2012 |
Ceriotti M, Diedrich BL, McInnes CR. Novel mission concepts for polar coverage: An overview of recent developments and possible future applications Acta Astronautica. 80: 89-104. DOI: 10.1016/J.Actaastro.2012.04.043 |
0.444 |
|
2012 |
Heiligers J, Ceriotti M, McInnes CR, Biggs JD. Design of optimal earth pole-sitter transfers using low-thrust propulsion Acta Astronautica. 79: 253-268. DOI: 10.1016/J.Actaastro.2012.04.025 |
0.47 |
|
2012 |
Lücking C, Colombo C, McInnes CR. A passive satellite deorbiting strategy for medium earth orbit using solar radiation pressure and the J 2 effect Acta Astronautica. 77: 197-206. DOI: 10.1016/J.Actaastro.2012.03.026 |
0.482 |
|
2012 |
Colombo C, McInnes C. Orbit design for future SpaceChip swarm missions in a planetary atmosphere Acta Astronautica. 75: 25-41. DOI: 10.1016/J.Actaastro.2012.01.004 |
0.45 |
|
2012 |
Sanchez JP, McInnes CR. Assessment on the feasibility of future shepherding of asteroid resources Acta Astronautica. 73: 49-66. DOI: 10.1016/J.Actaastro.2011.12.010 |
0.407 |
|
2012 |
Heiligers J, McInnes CR, Biggs JD, Ceriotti M. Displaced geostationary orbits using hybrid low-thrust propulsion Acta Astronautica. 71: 51-67. DOI: 10.1016/J.Actaastro.2011.08.012 |
0.451 |
|
2012 |
Ceriotti M, McInnes CR. Natural and sail-displaced doubly-symmetric Lagrange point orbits for polar coverage Celestial Mechanics and Dynamical Astronomy. 114: 151-180. DOI: 10.1007/S10569-012-9422-2 |
0.502 |
|
2011 |
Bennet DJ, McInnes C, Suzuki M, Uchiyama K. Autonomous three-dimensional formation flight for a swarm of unmanned aerial vehicles Journal of Guidance Control and Dynamics. 34: 1899-1908. DOI: 10.2514/1.53931 |
0.312 |
|
2011 |
Heiligers J, Ceriotti M, McInnes CR, Biggs JD. Displaced geostationary orbit design using hybrid sail propulsion Journal of Guidance, Control, and Dynamics. 34: 1852-1866. DOI: 10.2514/1.53807 |
0.488 |
|
2011 |
Macdonald M, Mckay RJ, Vasile M, Frescheville FBD, Biggs JD, Mcinnes C. Low-Thrust-Enabled Highly-Non-Keplerian Orbits in Support of Future Mars Exploration Journal of Guidance Control and Dynamics. 34: 1396-1411. DOI: 10.2514/1.52602 |
0.489 |
|
2011 |
Colombo C, McInnes C. Orbital dynamics of "Smart-Dust" devices with solar radiation pressure and drag Journal of Guidance, Control, and Dynamics. 34: 1613-1631. DOI: 10.2514/1.52140 |
0.448 |
|
2011 |
McKay RJ, MacDonald M, Biggs J, McInnes C. Survey of highly-non-Keplerian orbits with low-thrust propulsion Journal of Guidance, Control, and Dynamics. 34: 645-666. DOI: 10.2514/1.52133 |
0.472 |
|
2011 |
Ceriotti M, McInnes CR. Generation of optimal trajectories for Earth hybrid pole sitters Journal of Guidance, Control, and Dynamics. 34: 847-859. DOI: 10.2514/1.50935 |
0.489 |
|
2011 |
Sanchez JP, McInnes C. Asteroid resource map for near-Earth space Journal of Spacecraft and Rockets. 48: 153-165. DOI: 10.2514/1.49851 |
0.43 |
|
2011 |
Suzuki M, Uchiyama K, Bennet DJ, McInnes C. Three-dimensional formation flight for UAV using bifurcating velocity field Journal of the Japan Society For Aeronautical and Space Sciences. 59: 259-265. DOI: 10.2322/Jjsass.59.259 |
0.305 |
|
2011 |
Li M, Jing W, Macdonald M, McInnes CR. Adaptive Backstepping Control for Optimal Descent with Embedded Autonomy Aerospace Science and Technology. 15: 589-594. DOI: 10.1016/J.Ast.2010.12.002 |
0.302 |
|
2011 |
MacDonald M, McInnes C. Solar sail science mission applications and advancement Advances in Space Research. 48: 1702-1716. DOI: 10.1016/J.Asr.2011.03.018 |
0.381 |
|
2011 |
Ceriotti M, McInnes CR. Systems design of a hybrid sail pole-sitter Advances in Space Research. 48: 1754-1762. DOI: 10.1016/J.Asr.2011.02.010 |
0.431 |
|
2011 |
Ceriotti M, McInnes CR. Hybrid solar sail and solar electric propulsion for novel Earth observation missions Acta Astronautica. 69: 809-821. DOI: 10.1016/J.Actaastro.2011.06.007 |
0.504 |
|
2011 |
McInnes CR. Displaced non-Keplerian orbits using impulsive thrust Celestial Mechanics and Dynamical Astronomy. 110: 199-215. DOI: 10.1007/S10569-011-9351-5 |
0.396 |
|
2011 |
Biggs JD, Waters T, McInnes C. New periodic orbits in the solar sail three-body problem Nonlinear Science and Complexity. 131-138. DOI: 10.1007/978-90-481-9884-9_17 |
0.364 |
|
2010 |
Colombo C, McInnes C. Orbital dynamics of Earth-orbiting 'smart dust' spacecraft under the effects of solar radiation pressure and aerodynamic drag Aiaa/Aas Astrodynamics Specialist Conference 2010. DOI: 10.2514/6.2010-7656 |
0.367 |
|
2010 |
Baig S, McInnes CR. Light-Levitated Geostationary Cylindrical Orbits Are Feasible Journal of Guidance Control and Dynamics. 33: 782-793. DOI: 10.2514/1.46681 |
0.463 |
|
2010 |
Macdonald M, McInnes C, Hughes G. Technology requirements of exploration beyond Neptune by solar sail propulsion Journal of Spacecraft and Rockets. 47: 472-483. DOI: 10.2514/1.46657 |
0.409 |
|
2010 |
Biggs JD, McInnes CR. Passive orbit control for space-based geo-engineering Journal of Guidance, Control, and Dynamics. 33: 1017-1020. DOI: 10.2514/1.46054 |
0.446 |
|
2010 |
Brown B, McInnes C, Allouis E. Dynamic intelligent autonomous control of an asteroid lander Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 224: 865-879. DOI: 10.1243/09544100Jaero724 |
0.328 |
|
2009 |
Biggs J, McInnes CR. An optimal gains matrix for time-delay feedback control Ifac Proceedings Volumes. 42: 339-342. DOI: 10.3182/20090622-3-Uk-3004.00063 |
0.407 |
|
2009 |
Simo J, McInnes CR. Asymptotic analysis of displaced lunar orbits Journal of Guidance, Control, and Dynamics. 32: 1666-1670. DOI: 10.2514/1.43703 |
0.468 |
|
2009 |
Biggs JD, McInnes CR. Time-delayed feedback control in astrodynamics Journal of Guidance, Control, and Dynamics. 32: 1804-1811. DOI: 10.2514/1.43672 |
0.404 |
|
2009 |
Biggs JD, McInnes CR. Solar sail formation flying for deep-space remote sensing Journal of Spacecraft and Rockets. 46: 670-678. DOI: 10.2514/1.42404 |
0.482 |
|
2009 |
Biggs JD, McInnes CR, Waters T. Control of solar sail periodic orbits in the elliptic three-body problem Journal of Guidance, Control, and Dynamics. 32: 318-320. DOI: 10.2514/1.38362 |
0.494 |
|
2009 |
Bennet DJ, McInnes CR. Verifiable control of a swarm of unmanned aerial vehicles Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 223: 939-953. DOI: 10.1243/09544100Jaero508 |
0.317 |
|
2009 |
Simo J, McInnes CR. Solar sail orbits at the Earth–Moon libration points Communications in Nonlinear Science and Numerical Simulation. 14: 4191-4196. DOI: 10.1016/J.Cnsns.2009.03.032 |
0.514 |
|
2009 |
Badawy A, McInnes CR. Small spacecraft formation using potential functions Acta Astronautica. 65: 1783-1788. DOI: 10.1016/J.Actaastro.2009.05.002 |
0.37 |
|
2009 |
Baig S, McInnes CR. Artificial halo orbits for low-thrust propulsion spacecraft Celestial Mechanics and Dynamical Astronomy. 104: 321-335. DOI: 10.1007/S10569-009-9215-4 |
0.45 |
|
2008 |
Baig S, McInnes CR. Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion Journal of Guidance Control and Dynamics. 31: 1644-1655. DOI: 10.2514/1.36125 |
0.458 |
|
2008 |
Waters TJ, McInnes CR. Invariant Manifolds and Orbit Control in the Solar Sail Three-Body Problem Journal of Guidance Control and Dynamics. 31: 554-562. DOI: 10.2514/1.32292 |
0.453 |
|
2008 |
Badawy A, McInnes CR. On-orbit assembly using superquadric potential fields Journal of Guidance, Control, and Dynamics. 31: 30-43. DOI: 10.2514/1.28865 |
0.33 |
|
2008 |
Waters TJ, McInnes CR. Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits International Journal of Non-Linear Mechanics. 43: 490-496. DOI: 10.1016/J.Ijnonlinmec.2008.01.001 |
0.434 |
|
2008 |
Bookless J, McInnes C. Control of Lagrange point orbits using solar sail propulsion Acta Astronautica. 62: 159-176. DOI: 10.1016/J.Actaastro.2006.12.051 |
0.445 |
|
2007 |
Waters TJ, McInnes CR. Periodic orbits above the ecliptic in the solar-sail restricted three-body problem Journal of Guidance, Control, and Dynamics. 30: 687-693. DOI: 10.2514/1.26232 |
0.463 |
|
2007 |
McInnes CR. Near earth object orbit modification using gravitational coupling Journal of Guidance, Control, and Dynamics. 30: 870-873. DOI: 10.2514/1.25864 |
0.421 |
|
2007 |
Lappas V, Wie B, McInnes C, Tarabini L, Gomes L, Wallace K. Microsolar sails for earth magnetotail monitoring Journal of Spacecraft and Rockets. 44: 840-848. DOI: 10.2514/1.23456 |
0.447 |
|
2007 |
Macdonald M, Hughes GW, McInnes C, Lyngvi A, Falkner P, Atzei A. GeoSail: an elegant solar sail demonstration mission Journal of Spacecraft and Rockets. 44: 784-796. DOI: 10.2514/1.22867 |
0.442 |
|
2007 |
Dachwald B, Macdonald M, McInnes CR, Mengali G, Quarta AA. Impact of Optical Degradation on Solar Sail Mission Performance Journal of Spacecraft and Rockets. 44: 740-749. DOI: 10.2514/1.21432 |
0.377 |
|
2007 |
Macdonald M, McInnes CR, Dachwald B. Heliocentric Solar Sail Orbit Transfers with Locally Optimal Control Laws Journal of Spacecraft and Rockets. 44: 273-276. DOI: 10.2514/1.17297 |
0.468 |
|
2006 |
Baoyin H, McInnes CR. Trajectories to and from the lagrange points and the primary body surfaces Journal of Guidance, Control, and Dynamics. 29: 998-1003. DOI: 10.2514/1.17757 |
0.382 |
|
2006 |
Macdonald M, Hughes GW, McInnes CR, Lyngvi A, Falkner P, Atzei A. Solar Polar Orbiter: A Solar Sail Technology Reference Study Journal of Spacecraft and Rockets. 43: 960-972. DOI: 10.2514/1.16408 |
0.435 |
|
2006 |
Hughes GW, Macdonald M, McInnes CR, Atzei A, Falkner P. Sample return from Mercury and other terrestrial planets using solar sail propulsion Journal of Spacecraft and Rockets. 43: 828-835. DOI: 10.2514/1.15889 |
0.464 |
|
2006 |
Bookless J, McInnes C. Dynamics and control of displaced periodic orbits using solar-sail propulsion Journal of Guidance, Control, and Dynamics. 29: 527-537. DOI: 10.2514/1.15655 |
0.504 |
|
2006 |
Baoyin H, McInnes CR. Solar sail equilibria in the elliptical restricted three-body problem Journal of Guidance, Control, and Dynamics. 29: 538-543. DOI: 10.2514/1.15596 |
0.404 |
|
2006 |
Macdonald M, McInnes C, Alexander D, Sandman A. GeoSail: Exploring the magnetosphere using a low-cost solar sail Acta Astronautica. 59: 757-767. DOI: 10.1016/J.Actaastro.2005.07.023 |
0.434 |
|
2006 |
Hughes GW, Macdonald M, McInnes CR, Atzei A, Falkner P. Terrestrial planet sample return missions using solar sail propulsion Acta Astronautica. 59: 797-806. DOI: 10.1016/J.Actaastro.2005.07.019 |
0.339 |
|
2006 |
Baoyin H, Mcinnes CR. Solar sail halo orbits at the Sun-Earth artificial L1 point Celestial Mechanics and Dynamical Astronomy. 94: 155-171. DOI: 10.1007/S10569-005-4626-3 |
0.397 |
|
2005 |
Macdonald M, McInnes CR. Realistic Earth escape strategies for solar sailing Journal of Guidance Control and Dynamics. 28: 315-323. DOI: 10.2514/1.5165 |
0.457 |
|
2005 |
Baoyin H, McInnes CR. Solar sail orbits at artificial Sun-Earth libration points Journal of Guidance Control and Dynamics. 28: 1328-1331. DOI: 10.2514/1.14598 |
0.496 |
|
2005 |
McInnes CR. Dynamics of a Particle Moving Along an Orbital Tower Journal of Guidance Control and Dynamics. 28: 380-382. DOI: 10.2514/1.13505 |
0.361 |
|
2005 |
Macdonald M, McInnes CR. Spacecraft planetary capture using gravity-assist maneuvers Journal of Guidance Control and Dynamics. 28: 365-369. DOI: 10.2514/1.11866 |
0.393 |
|
2005 |
Macdonald M, McInnes CR. Analytical Control Laws for Planet-Centered Solar Sailing Journal of Guidance Control and Dynamics. 28: 1038-1048. DOI: 10.2514/1.11400 |
0.464 |
|
2005 |
Umehara H, McInnes CR. Penalty-Function Guidance for Multiple-Satellite Cluster Formation Journal of Guidance Control and Dynamics. 28: 182-185. DOI: 10.2514/1.10677 |
0.317 |
|
2004 |
Hughes GW, McInnes CR. Small-Body Encounters Using Solar Sail Propulsion Journal of Spacecraft and Rockets. 41: 140-150. DOI: 10.2514/1.9277 |
0.445 |
|
2004 |
McInnes CR. Deflection of near-Earth asteroids by kinetic energy impacts from retrograde orbits Planetary and Space Science. 52: 587-590. DOI: 10.1016/J.Pss.2003.12.010 |
0.433 |
|
2004 |
McInnes CR. Delivering fast and capable missions to the outer solar system Advances in Space Research. 34: 184-191. DOI: 10.1016/J.Asr.2003.02.063 |
0.438 |
|
2003 |
McInnes CR. Solar Sailing: Mission Applications and Engineering Challenges Philosophical Transactions of the Royal Society a: Mathematical, Physical and Engineering Sciences. 361: 2989-3008. PMID 14667309 DOI: 10.1098/Rsta.2003.1280 |
0.468 |
|
2003 |
McInnes CR. Orbits in a generalized two-body problem Journal of Guidance Control and Dynamics. 26: 743-749. DOI: 10.2514/2.5129 |
0.337 |
|
2003 |
McInnes CR. Azimuthal repositioning of payloads in heliocentric orbit using solar sails Journal of Guidance Control and Dynamics. 26: 662-664. DOI: 10.2514/2.5098 |
0.488 |
|
2003 |
McInnes CR. Instability of Fixed, Low-Thrust Drag Compensation Journal of Guidance Control and Dynamics. 26: 655-657. DOI: 10.2514/2.5094 |
0.385 |
|
2003 |
McInnes CR. Inverse solar sail trajectory problem Journal of Guidance Control and Dynamics. 26: 369-371. DOI: 10.2514/2.5057 |
0.489 |
|
2003 |
McInnes CR. Gravity-turn descent from low circular orbit conditions Journal of Guidance Control and Dynamics. 26: 183-185. DOI: 10.2514/2.5033 |
0.386 |
|
2003 |
McInnes C, Hughes GW, Macdonald M. Low cost Mercury orbiter and Mercury sample return missions using solar sail propulsion Aeronautical Journal. 107: 469-478. DOI: 10.1017/S0001924000013385 |
0.436 |
|
2003 |
McInnes CR. Solar sailing: Orbital mechanics and mission applications Advances in Space Research. 31: 1971-1980. DOI: 10.1016/S0273-1177(03)00172-8 |
0.46 |
|
2002 |
Hughes GW, McInnes CR. Solar Sail Hybrid Trajectory Optimization for Non-Keplerian Orbit Transfers Journal of Guidance Control and Dynamics. 25: 602-604. DOI: 10.2514/2.4924 |
0.495 |
|
2002 |
McInnes CR, Hughes G, MacDonald M. Payload Mass Fraction Optimization for Solar Sail Cargo Missions Journal of Spacecraft and Rockets. 39: 933-935. DOI: 10.2514/2.3901 |
0.475 |
|
2002 |
McInnes CR. Astronomical engineering revisited: Planetary orbit modification using solar radiation pressure Astrophysics and Space Science. 282: 765-772. DOI: 10.1023/A:1021178603836 |
0.447 |
|
2001 |
Otten M, McInnes CR. Near Minimum-Time Trajectories for Solar Sails Journal of Guidance Control and Dynamics. 24: 632-634. DOI: 10.2514/2.4758 |
0.424 |
|
2001 |
McInnes CR, Macdonald M, Angelopoulos V, Alexander D. GEOSAIL: Exploring the Geomagnetic Tail Using a Small Solar Sail Journal of Spacecraft and Rockets. 38: 622-629. DOI: 10.2514/2.3727 |
0.456 |
|
2001 |
McInnes CR. Advances in space systems engineering at the University of Glasgow Aircraft Engineering and Aerospace Technology. 73: 360-366. DOI: 10.1108/00022660110399399 |
0.316 |
|
2000 |
Roger AB, McInnes CR. Safety Constrained Free-Flyer Path Planning at the International Space Station Journal of Guidance Control and Dynamics. 23: 971-979. DOI: 10.2514/2.4656 |
0.342 |
|
2000 |
McInnes CR. Simple Analytic Model of the Long-Term Evolution of Nanosatellite Constellations Journal of Guidance Control and Dynamics. 23: 332-338. DOI: 10.2514/2.4527 |
0.303 |
|
1999 |
McInnes CR. Artificial Lagrange Points for a Partially Reflecting Flat Solar Sail Journal of Guidance Control and Dynamics. 22: 185-187. DOI: 10.2514/2.7627 |
0.392 |
|
1999 |
Gillies EA, Johnston AGY, McInnes CR. Action Selection Algorithms for Autonomous Microspacecraft Journal of Guidance Control and Dynamics. 22: 914-916. DOI: 10.2514/2.4473 |
0.36 |
|
1999 |
McInnes CR. Solar sail mission applications for non-Keplerian orbits Acta Astronautica. 45: 567-575. DOI: 10.1016/S0094-5765(99)00177-0 |
0.479 |
|
1998 |
McInnes CR. Passive Control of Displaced Solar Sail Orbits Journal of Guidance Control and Dynamics. 21: 975-982. DOI: 10.2514/2.4334 |
0.457 |
|
1998 |
McInnes CR. Dynamics, Stability, and Control of Displaced Non-Keplerian Orbits Journal of Guidance Control and Dynamics. 21: 799-805. DOI: 10.2514/2.4309 |
0.439 |
|
1997 |
McInnes CR. Low-Thrust Orbit Raising with Coupled Plane Change and J Precession Journal of Guidance Control and Dynamics. 20: 607-609. DOI: 10.2514/2.4084 |
0.314 |
|
1997 |
Mcinnes CR. The Existence and Stability of Families of Displacement Two-Body Orbits Celestial Mechanics and Dynamical Astronomy. 67: 167-180. DOI: 10.1023/A:1008280609889 |
0.396 |
|
1997 |
Mcquade F, Mcinnes CR. Autonomous control for on-orbit assembly using potential function methods Aeronautical Journal. 101: 255-262. DOI: 10.1017/S0001924000066288 |
0.332 |
|
1996 |
McInnes CR, Radice G. Line-Of-Sight Guidance For Descent To A Minor Solar System Body Journal of Guidance Control and Dynamics. 19: 740-742. DOI: 10.2514/3.21693 |
0.345 |
|
1996 |
McInnes CR. Nonlinear transformation methods for gravity-turn descent Journal of Guidance Control and Dynamics. 19: 247-248. DOI: 10.2514/3.21607 |
0.309 |
|
1995 |
McInnes CR. Distributed control of maneuvering vehicles for on-orbit assembly Journal of Guidance Control and Dynamics. 18: 1204-1206. DOI: 10.2514/3.21526 |
0.322 |
|
1995 |
Lopez I, McInnes CR. Autonomous rendezvous using artificial potential function guidance Journal of Guidance Control and Dynamics. 18: 237-241. DOI: 10.2514/3.21375 |
0.313 |
|
1995 |
McInnes CR. Solar sail spacecraft Historical development and mission applications Interdisciplinary Science Reviews. 20: 289-301. DOI: 10.1179/030801895794105415 |
0.302 |
|
1995 |
McInnes CR. Path shaping guidance for terminal lunar descent Acta Astronautica. 36: 367-377. DOI: 10.1016/0094-5765(95)00119-0 |
0.328 |
|
1994 |
McInnes CR. Large angle slew maneuvers with autonomous sun vector avoidance Journal of Guidance Control and Dynamics. 17: 875-877. DOI: 10.2514/3.21283 |
0.306 |
|
1994 |
McInnes CR, McDonald AJC, Simmons JFL, MacDonald EW. Solar sail parking in restricted three-body systems Journal of Guidance Control and Dynamics. 17: 399-406. DOI: 10.2514/3.21211 |
0.397 |
|
1994 |
McInnes CR. Compact analytic solutions for a decaying, precessing circular orbit Aeronautical Journal. 98: 357-360. DOI: 10.1017/S0001924000026920 |
0.319 |
|
1994 |
McInnes CR. Aero-assisted trajectories for direct launch systems Acta Astronautica. 32: 411-417. DOI: 10.1016/0094-5765(94)90042-6 |
0.432 |
|
1993 |
McInnes CR. Solar sail trajectories at the lunar L2 Lagrange point Journal of Spacecraft and Rockets. 30: 782-784. DOI: 10.2514/3.26393 |
0.35 |
|
1992 |
McInnes CR, Simmons JFL. Solar Sail Halo Orbits II: Geocentric Case Journal of Spacecraft and Rockets. 29: 472-479. DOI: 10.2514/3.55639 |
0.448 |
|
1991 |
McInnes CR. Solar sailing: a new tool for solar system research Vistas in Astronomy. 34: 369-408. DOI: 10.1016/0083-6656(91)90026-O |
0.448 |
|
1990 |
Mcinnes CR, Brown JC. Terminal velocity of a laser-driven light sail Journal of Spacecraft and Rockets. 27: 48-52. DOI: 10.2514/3.26104 |
0.519 |
|
1990 |
McInnes CR, Brown JC. Solar sail dynamics with an extended source of radiation pressure Acta Astronautica. 22: 155-160. DOI: 10.1016/0094-5765(90)90017-F |
0.597 |
|
1990 |
McInnes CR, Brown JC. The dynamics of solar sails with a non-point source of radiation pressure Celestial Mechanics and Dynamical Astronomy. 49: 249-264. DOI: 10.1007/Bf00049416 |
0.59 |
|
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