Zobrazeno 1 - 10
of 13
pro vyhledávání: '"H. N. Suresha Kumar"'
Publikováno v:
Journal of Spacecraft and Rockets. 60:190-198
Camera steering mechanisms have been extensively used in the International Space Station; rovers of interplanetary missions; and humanoids for surveillance, path planning, and experimentation. Based on the application, both stereoscopic and planar im
Autor:
Abhinandan Kapoor, H N Suresha Kumar, Gaurav Sharma, Girish Anantapur, Gaurav Saxena, Kalpana Arvind, Abhishek Kumar, null DineshBVS
Publikováno v:
Advances in Space Research. 70:3450-3465
Autor:
Abhinandan Kapoor, B. P. Nagaraj, Abhishek Kumar, H. N. Suresha Kumar, B. V. S. Dinesh, N. Viswanatha, D. Manoj Reddy, Sidharth Tiwary, A. Shankara, K Prakasha, B. K. Muthu
Publikováno v:
CEAS Space Journal.
Autor:
Amit Kamboj, null Aditya, Anoop Kumar Srivastava, K. Balaji, Abhishek Kumar, B. P. Nagaraj, H. N. Suresha Kumar, Alok Kumar Shrivastava
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9789811971976
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db04d6963af19c8900a27e30c38da23e
https://doi.org/10.1007/978-981-19-7198-3_12
https://doi.org/10.1007/978-981-19-7198-3_12
Autor:
V. Sri Pavan Ravichand, Divesh Soni, Sanjay Gorur, Ghulam Sarwar, null Shamrao, B. Lakshmi Narayana, S. Narendra, B. P. Nagaraj, H. N. Suresha Kumar
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811937156
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f5b53eadf6056a85f5b8d44d252c9e3
https://doi.org/10.1007/978-981-19-3716-3_34
https://doi.org/10.1007/978-981-19-3716-3_34
Publikováno v:
Materials Today: Proceedings. 28:2463-2470
Deployable space structures have always fascinated space scientist and engineers. They serve the purpose of compact packaging volume during launch and a large deployed length in space subsequent to satellite ejection in orbit. Booms are any kind of d
Autor:
A. Shankara, V. Sri Pavan Ravichand, Anoop Kumar Srivastava, Saurabhkumar H. Patel, H. N. Suresha Kumar, S. Narendra
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811617683
The Hold-down system is a key unit on satellite that enables rigid holding of antenna on to the spacecraft structure so as to withstand diverse loads during launch. The hold-down system gets released on orbit upon actuation command so that the antenn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ae6c663bc98fa9a8ceb6f275ba87c78
https://doi.org/10.1007/978-981-16-1769-0_9
https://doi.org/10.1007/978-981-16-1769-0_9
Autor:
H. N. Suresha Kumar, Abhishek Kumar, Anoop Kumar Srivastava, V. Sri Pavan Ravichand, K. A. Keshavamurthy
Publikováno v:
Advances in Mechanical Engineering ISBN: 9789811536380
Mechanism for gimballing of antenna on-orbit is a critical appendage on any satellite. It is necessary for directed beam data transfer from satellite to ground stations. For near-real-time data transfer, the dual-axis steering of the antenna is requi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f25c3e0b194ec7ea3042ef623563a0b
https://doi.org/10.1007/978-981-15-3639-7_62
https://doi.org/10.1007/978-981-15-3639-7_62
Autor:
Gaurav Sharma, Abhinandan Kapoor, KN Sajeesh, Subash Yadav, K. A. Keshavamurthy, N. Viswanatha, H. N. Suresha Kumar
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:2610-2625
Astronomical payloads for monitoring of X-rays from planetary bodies require an active filter wheel drive mechanism to control the energy threshold, encompassing a larger range of solar X-ray intensity. If the detector aperture in the monitoring inst
Publikováno v:
Journal of Terramechanics. 76:39-52
Low mass compact rovers provide cost effective means to explore extra-terrestrial terrains. Use of flexible wheels in such applications where the wheel size is restricted, improves traction at reduced slip and sinkage. Design of a flexible wheel for