| Orbit Theory with Lunar Perturbation in Terms of Kustaanheimo–Stiefel Regular Elements H Sellamuthu, RK Sharma Journal of Guidance, Control, and Dynamics 40 (5), 1272-1277, 2017 | 9 | 2017 |
| Hybrid orbit propagator for small spacecraft using Kustaanheimo-Stiefel elements H Sellamuthu, RK Sharma Journal of Spacecraft and Rockets 55 (5), 1282-1288, 2018 | 7 | 2018 |
| Regularized luni-solar gravity dynamics on resident space objects H Sellamuthu, RK Sharma Astrodynamics 5, 91-108, 2021 | 5 | 2021 |
| Perturbed Trojan Dynamics in the Solar system RK Sharma, H Sellamuthu, A Jency AAS/AIAA Astrodynamics Specialist Conference, 2020 | 3 | 2020 |
| On J2 short-term orbit predictions in terms of KS elements SS Saji, H Sellamuthu, RK Sharma International Journal of Advanced Astronomy 5 (1), 7-11, 2017 | 2 | 2017 |
| An Analytical Theory with Respect to the Earth’s Zonal Harmonic Term J2 in Terms of Eccentric Anomaly for Short-Term Orbit Predictions MJ Smibi, H Sellamuthu, RK Sharma Advances in Astrophysics 2, 141-150, 2017 | 1 | 2017 |
| Regularized orbit observability for resident space objects H Sellamuthu 43rd COSPAR Scientific Assembly. Held 28 January-4 February 43, 2204, 2021 | | 2021 |
| Regularized analytical orbit theory with solar radiation pressure H Sellamuthu, RK Sharma, N Pushparaj, S Ravichandran, ... 71st International Astronautical Congress (IAC) – The CyberSpace Edition, 2020 | | 2020 |
| Sun Gravity-Assist to Trans-Lunar Injection Orbits H Sellamuthu, S Arumugam, S RK Lecture Notes in Mechanical Engineering 112, 1-10, 2020 | | 2020 |
| Optimized re-entry time prediction of Molniya orbit objects H Sellamuthu, RK Sharma, BJ Solomon, S Ravichandran, ... 70th International Astronautical Congress, 2019 | | 2019 |
| Regularized Astrodynamics using Kustaanheimo-Stiefel space H Sellamuthu Karunya Institute of Technology and Sciences, 2019 | | 2019 |
| Sun gravity-assist to trans-lunar injection orbits H Sellamuthu, S Arumugam, RK Sharma 63rd Congress of the Indian Society for Theoretical and Applied Mechanics,, 2018 | | 2018 |
| Optimal Re-entry Time Prediction Of Resident Space Objects from Highly Elliptical Orbits H Sellamuthu SPACE, 2018 | | 2018 |
| On-Board Orbit Propagator Using Kustaanheimo-Stiefel Elements for Mars Micro Orbiters H Sellamuthu, RK Sharma 3rd International Workshop on Instrumentation for Planetary Missions, 2016 | | 2016 |
| Orbital theory in terms of KS elements with luni-solar perturbations H Sellamuthu, R Sharma 41st COSPAR Scientific Assembly 41, PSD. 1-9-16, 2016 | | 2016 |
| Orbit Predictions of High Eccentricity Satellite Orbits with Luni-Solar Effects Using KS Elements H Sellamuthu, AA Jeevi, RK Sharma, S Rekh 66th International Astronautical Congress, 2015 | | 2015 |
| ANALYTICAL THEORY USING KS ELEMENTS FOR ORBIT PREDICTION WITH SOLAR GRAVITATION PERTURBATION H Sellamuthu, RK Sharma ISTAM 2014, 2014 | | 2014 |
