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Mars Entry Mission Bank Profile Optimization

Journal of guidance, control, and dynamics, 2014-07, Vol.37 (4), p.1305-1316

2014

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Solid-State Circuit Breaker Protection for DC Shipboard Power Systems: Breaker Design, Protection Scheme, Validation Testing

IEEE transactions on industry applications, 2020-03, Vol.56 (2), p.952-960

2020

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Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution

Advances in space research, 2016-01, Vol.57 (1), p.202-217

2016

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Optimal low-thrust GTO–GSO transfers using differential evolution

Sadhana (Bangalore), 2021-12, Vol.46 (1), Article 1

2021

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Design of multi-revolution orbits in the framework of elliptic restricted three-body problem using differential evolution

Journal of astrophysics and astronomy, 2021-12, Vol.42 (1), Article 5

2021

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Analysis of optimal strategies for soft landing on the Moon from lunar parking orbits

Journal of Earth System Science, 2005-12, Vol.114 (6), p.807-813

2005

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Direct Interplanetary Trajectory Design Using a Precise V-Infinity Targeting Technique

Journal of guidance, control, and dynamics, 2018-10, Vol.41 (10), p.2293-2299

2018

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Iterative Pseudostate Method for Transfer Trajectory Design of Interplanetary Orbiter Missions

Journal of guidance, control, and dynamics, 2016-12, Vol.39 (12), p.2799-2809

2016

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A Novel Indirect Scheme for Optimal Lunar Soft Landing at a Target Site

Journal of the Institution of Engineers (India) Series C, 2021-12, Vol.102 (6), p.1379-1393

2021

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Nonimpact Lunar Transfer Trajectories Using the Pseudostate Technique

Journal of guidance, control, and dynamics, 2005-03, Vol.28 (2), p.217-225

2005

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Integrated Algorithm for Lunar Transfer Trajectories Using a Pseudostate Technique

Journal of guidance, control, and dynamics, 2002-09, Vol.25 (5), p.946-952

Ramanan, R. V

2002

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Precise Lunar Gravity Assist Transfers to Geostationary Orbits

Journal of guidance, control, and dynamics, 2006-03, Vol.29 (2), p.500-502

2006

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The kinetics of nanocrystallization and microstructural observations in FINEMET, NANOPERM and HITPERM nanocomposite magnetic materials

Scripta materialia, 2003-04, Vol.48 (7), p.881-887

2003

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An analysis of near-circular lunar mapping orbits

Journal of Earth System Science, 2005-12, Vol.114 (6), p.619-626

2005

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Fuel Optimum Lunar Soft Landing Trajectory Design Using Different Solution Schemes

International Review of Aerospace Engineering (IREASE), 2016, Vol.9 (5), p.131

2016

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Ectopic Pregnancy - the Leash Sign. A New Sign on Transvaginal Doppler Ultrasound

Acta radiologica (1987), 2006-06, Vol.47 (5), p.529-535

2006

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SSCB Protection for DC Shipboard Power Systems: Breaker Design, Protection Scheme, Validation Testing

2019 IEEE Industry Applications Society Annual Meeting, 2019, p.1-8

2019

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Design and analysis of quasi-halo orbits and optimal transfers from the Earth under different Sun–Earth frameworks using differential evolution

Journal of astrophysics and astronomy, 2023-08, Vol.44 (2), Article 81

2023

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Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm

Journal of Earth System Science, 2005-12, Vol.114 (6), p.711-716

2005

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High Current Solid State Circuit Breaker for DC Shipboard Power Systems

2019 IEEE Electric Ship Technologies Symposium (ESTS), 2019, p.468-476

2019

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Two-impulse transfer to multi-revolution halo orbits in the Earth–Moon elliptic restricted three body problem framework

Journal of astrophysics and astronomy, 2022-08, Vol.43 (2), Article 50

2022

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Fuel-optimal and Energy-optimal guidance schemes for lunar soft landing at a desired location

Advances in space research, 2021-03, Vol.67 (6), p.1787-1804

2021

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Strategy for Deployment of Multiple Satellites for Collision-Free Relative Orbital Motion

Journal of guidance, control, and dynamics, 2000-05, Vol.23 (3), p.556-558

Ramanan, R. V

2000

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Halo orbit design around Lagrangian points using gradient and non gradient based optimization techniques

AIP Conference Proceedings, 2018, Vol.1975 (1)

2018

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Modulation of Aerodynamic Angles for Optimal Mars Descent Trajectory using Indirect Approach

Advances in astronautics science and technology (Online), 2020-12, Vol.3 (2), p.133-143

2020

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Mars Entry Mission Bank Profile Optimization

Solid-State Circuit Breaker Protection for DC Shipboard Power Systems: Breaker Design, Protection Scheme, Validation Testing

Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution

Optimal low-thrust GTO–GSO transfers using differential evolution

Design of multi-revolution orbits in the framework of elliptic restricted three-body problem using differential evolution

Analysis of optimal strategies for soft landing on the Moon from lunar parking orbits

Direct Interplanetary Trajectory Design Using a Precise V-Infinity Targeting Technique

Iterative Pseudostate Method for Transfer Trajectory Design of Interplanetary Orbiter Missions

A Novel Indirect Scheme for Optimal Lunar Soft Landing at a Target Site

Nonimpact Lunar Transfer Trajectories Using the Pseudostate Technique

Integrated Algorithm for Lunar Transfer Trajectories Using a Pseudostate Technique

Precise Lunar Gravity Assist Transfers to Geostationary Orbits

The kinetics of nanocrystallization and microstructural observations in FINEMET, NANOPERM and HITPERM nanocomposite magnetic materials

An analysis of near-circular lunar mapping orbits

Fuel Optimum Lunar Soft Landing Trajectory Design Using Different Solution Schemes

Ectopic Pregnancy - the Leash Sign. A New Sign on Transvaginal Doppler Ultrasound

SSCB Protection for DC Shipboard Power Systems: Breaker Design, Protection Scheme, Validation Testing

Design and analysis of quasi-halo orbits and optimal transfers from the Earth under different Sun–Earth frameworks using differential evolution

Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm

High Current Solid State Circuit Breaker for DC Shipboard Power Systems

Two-impulse transfer to multi-revolution halo orbits in the Earth–Moon elliptic restricted three body problem framework

Fuel-optimal and Energy-optimal guidance schemes for lunar soft landing at a desired location

Strategy for Deployment of Multiple Satellites for Collision-Free Relative Orbital Motion

Halo orbit design around Lagrangian points using gradient and non gradient based optimization techniques

Modulation of Aerodynamic Angles for Optimal Mars Descent Trajectory using Indirect Approach

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