105 citations
- A. Nandi21 · h 22
- V. K. Agrawal3 profiles19 · h 15
- K. Sankarasubramanian3 profiles12 · h 16
- P. Sreekumar2 profiles9 · h 45
- Santabrata Das8 · h 24
- T. Katoch7 · h 15
- D. Bhattacharya2 profiles6 · h 7
- Rwitika Chatterjee6 · h 5
- Anuj Nandi5
- A. R. Rao2 profiles5 · h 25
- H. Sreehari5 · h 8
- M. Ramadevi2 profiles5 · h 10
- Tata Institute of Fundamental ResearchIN17 papers
- Indian Institute of AstrophysicsIN16 papers
- Indian Institute of Space Science and TechnologyIN14 papers
- U. R. Rao Satellite CentreIN14 papers
- Indian Institute of Technology GuwahatiIN12 papers
- Inter-University Centre for Astronomy and AstrophysicsIN12 papers
- Indian Institute of Science BangaloreIN10 papers
- Indian Institute of Science Education and Research KolkataIN9 papers
- Physical Research LaboratoryIN8 papers
- University of CalicutIN8 papers
- Manipal Academy of Higher EducationIN7 papers
- Vikram Sarabhai Space CentreIN7 papers
14 papers · 1 filter
HEL1OS -- A Hard X-ray Spectrometer on Board Aditya-L1
Anuj Nandi, Manju Sudhakar, Srikar Paavan Tadepalli +33
HEL1OS (High Energy L1 Orbiting X-ray Spectrometer) is one of the remote sensing payloads on board Aditya-L1 mission designed to continuously monitor and measure the time-resolved…
Analysis of Optimal Thrust to Mass Ratio Requirement for Maximizing Payload Mass of Lunar Landing Mission
Aditya Rallapalli, Suraj Kumar, Rijesh MP +2
Recent successful lunar landing missions have generated significant interest among space agencies in establishing a permanent human settlement on the Moon. Building a lunar base re…
Solving Infinite-Horizon Optimal Control Problems using the Extreme Theory of Functional Connections
Tanay Raghunandan Srinivasa, Suraj Kumar
This paper presents a physics-informed machine learning approach for synthesizing optimal feedback control policy for infinite-horizon optimal control problems by solving the Hamil…
Learning based Modelling of Throttleable Engine Dynamics for Lunar Landing Mission
Suraj Kumar, Aditya Rallapalli, Bharat Kumar GVP
Typical lunar landing missions involve multiple phases of braking to achieve soft-landing. The propulsion system configuration for these missions consists of throttleable engines.…
Post Processing of image segmentation using Conditional Random Fields
Aashish Dhawan, Pankaj Bodani, Vishal Garg
The output of image the segmentation process is usually not very clear due to low quality features of Satellite images. The purpose of this study is to find a suitable Conditional…
Spectral nature of Sco X-1 observed using the X-ray SPECtroscopy and Timing (XSPECT) payload on-board XPoSat
V. P. Shyam Prakash, Vivek K. Agrawal, Rwitika Chatterjee +3
Scorpius X-1 is the brightest and first discovered X-ray source in the sky. Studying this source in the low-energy band has been challenging in the past due to its high brightness.…