| Analysis of optimal strategies for soft landing on the moon from lunar parking orbits RV Ramanan, M Lal Journal of earth system science 114, 807-813, 2005 | 60 | 2005 |
| An analysis of near-circular lunar mapping orbits RV Ramanan, V Adimurthy Journal of Earth System Science 114, 619-626, 2005 | 32 | 2005 |
| Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution P Nath, RV Ramanan Advances in Space Research 57 (1), 202-217, 2016 | 31 | 2016 |
| Mars entry mission bank profile optimization GL Jacob, G Neeler, RV Ramanan Journal of Guidance, Control, and Dynamics 37 (4), 1305-1316, 2014 | 27 | 2014 |
| Integrated algorithm for lunar transfer trajectories using a pseudostate technique RV Ramanan Journal of guidance, control, and dynamics 25 (5), 946-952, 2002 | 22 | 2002 |
| Nonimpact lunar transfer trajectories using the pseudostate technique RV Ramanan, V Adimurthy Journal of guidance, control, and dynamics 28 (2), 217-225, 2005 | 19 | 2005 |
| Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm V Adimurthy, RV Ramanan, SR Tandon, C Ravikumar Journal of earth system science 114, 711-716, 2005 | 18 | 2005 |
| Direct transfer trajectory design options for interplanetary orbiter missions using an iterative patched conic method SP Parvathi, RV Ramanan Advances in Space Research 59 (7), 1763-1774, 2017 | 13 | 2017 |
| Iterative pseudostate method for transfer trajectory design of interplanetary orbiter missions SP Parvathi, RV Ramanan Journal of Guidance, Control, and Dynamics 39 (12), 2799-2809, 2016 | 13 | 2016 |
| Fuel optimum lunar soft landing trajectory design using different solution schemes N Remesh, RV Ramanan, VR Lalithambika International Review of Aerospace Engineering (IREASE) 9 (5), 131, 2016 | 13 | 2016 |
| Optimum rendezvous transfer between coplanar heliocentric elliptic orbits using solar sail PVS Rao, RV Ramanan Journal of guidance, control, and dynamics 15 (6), 1507-1509, 1992 | 11 | 1992 |
| Precise lunar gravity assist transfers to geostationary orbits RV Ramanan, V Adimurthy Journal of guidance, control, and dynamics 29 (2), 500-502, 2006 | 9 | 2006 |
| Optimal three-dimensional heliocentric solar-sail rendezvous transfer trajectories PVS Rao, RV Ramanan Acta Astronautica 29 (5), 341-345, 1993 | 8 | 1993 |
| Design of multi-revolution orbits in the framework of elliptic restricted three-body problem using differential evolution R Neelakantan, RV Ramanan Journal of Astrophysics and Astronomy 42, 1-18, 2021 | 6 | 2021 |
| Fuel-optimal and Energy-optimal guidance schemes for lunar soft landing at a desired location N Remesh, RV Ramanan, VR Lalithambika Advances in Space Research 67 (6), 1787-1804, 2021 | 5 | 2021 |
| Design and Analysis Tool for Mars Atmospheric Entry Missions. JR Pillai, A John, RV Ramanan International Journal of Aerospace Innovations 5 (1), 2013 | 4 | 2013 |
| Optimal 3d lunar soft landing trajectory design and performance evaluation of explicit guidance laws N Remesh, RV Ramanan, VR Lalithambika 2017 First International Conference on Recent Advances in Aerospace …, 2017 | 3 | 2017 |
| Multiple design options for interplanetary orbiter missions using pseudostate technique SP Parvathi, RV Ramanan 26th AAS/AIAA Space Flight Mechanics Meeting, Napa, California, 2016 | 3 | 2016 |
| Multidisciplinary Optimization Aerospace Design: The Emerging Technology For Complex Systems V Adimurthy, R Balu, P Priyadarshi, RV Ramanan, C Ravikumar Journal of Aerospace Sciences and Technologies, 79-92, 2005 | 3 | 2005 |
| An iterative analytical technique for the design of interplanetary direct transfer trajectories including perturbations SP Parvathi, RV Ramanan Advances in Space Research 61 (12), 3002-3019, 2018 | 2 | 2018 |
