Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Harish K. Joglekar"'
Autor:
Harish K. Joglekar, Kakanuru Sumithra
Publikováno v:
IFAC-PapersOnLine. 53:99-104
Satellite imagery data generates huge revenue due to its numerous applications in various fields. This requires the imagery and earth observation satellites to perform frequent rapid maneuvers for capturing images of different locations on earth. Due
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::93f3565b74e6646e1920d5cc1f654657
https://doi.org/10.1016/j.ifacol.2020.06.017
https://doi.org/10.1016/j.ifacol.2020.06.017
Autor:
Jasvinder Singh Khoral, Manoj Kumar, R. Aditya, A. M. Nagalakshmi, Harish K. Joglekar, Deepa Pramod, Prashant Kulshreshtha
Publikováno v:
Journal of Astrophysics and Astronomy. 42
AstroSat is India’s first mission dedicated to space-based Astronomy and carries a complement of instruments sensitive over a wide spectral region covering visible, ultraviolet, soft X-ray and hard X-ray bands. The spacecraft platform provides the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::433a5fb7b1ac5bd4f69772a757cb5c64
https://doi.org/10.1007/s12036-021-09730-6
https://doi.org/10.1007/s12036-021-09730-6
Publikováno v:
IFAC-PapersOnLine. 49:118-123
Earth observation satellites require rapid attitude maneuvering and stringent pointing accuracy for imaging payloads. This paper presents a configuration with Control Moment Gyros (CMG) and Steering scheme for rapid maneuvering of Indian spacecrafts.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7757479e3071e9e8a789018998fe15a
https://doi.org/10.1016/j.ifacol.2016.03.039
https://doi.org/10.1016/j.ifacol.2016.03.039
Autor:
T. Nagamani, Chaitra Rao, R. Pandiyan, Naresh Kumar, Anshu Chauhan, S. V. Subbarao, B. P. Dakshayani, Surya Ratna Prakash Dumpa, Harish K. Joglekar, N. Hari Prasad Rao
Publikováno v:
Journal of Astrophysics and Astronomy. 38
On 28th September 2015, India launched its first astronomical space observatory AstroSat, successfully. AstroSat carried five astronomy payloads, namely, (i) Cadmium Zinc Telluride Imager (CZTI), (ii) Large Area X-ray Proportional Counter (LAXPC), (i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88efed2e072f148917e40a4427bc3e99
https://doi.org/10.1007/s12036-017-9446-9
https://doi.org/10.1007/s12036-017-9446-9
Publikováno v:
Systems & Control Letters. 47:355-364
This paper describes the swing-up and stabilization of a cart–pendulum system with a restricted cart track length and restricted control force using generalized energy control methods. Starting from a pendant position, the pendulum is swung up to t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::270c8c21f4ec427899657c426ea33763
https://doi.org/10.1016/s0167-6911(02)00229-3
https://doi.org/10.1016/s0167-6911(02)00229-3