Zobrazeno 1 - 10
of 63
pro vyhledávání: '"I.G. Sarma"'
Publikováno v:
Journal of Guidance, Control, and Dynamics. 17:1357-1363
A new form of the Proportional Navigation (PN) guidance law for short-range homing missiles is proposed. Named the Switched Bias Proportional Navigation (SBPN) law, it is derived by invoking sliding-mode control theory and is structured around the ba
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d20d52ac6e4cfb7189cc948900bf0ea
https://doi.org/10.2514/3.21356
https://doi.org/10.2514/3.21356
Publikováno v:
IndraStra Global.
A hybrid simulation technique for identification and steady state optimization of a tubular reactor used in ammonia synthesis is presented. The parameter identification program finds the catalyst activity factor and certain heat transfer coefficients
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3a9d487d5a2aa044d4c906e2db1a0a72
http://eprints.iisc.ac.in/42830/1/IDENTIFICATI.pdf
http://eprints.iisc.ac.in/42830/1/IDENTIFICATI.pdf
Publikováno v:
Journal of Guidance, Control, and Dynamics. 17:1389-1391
Homing guidance schemes based on fuzzy logic have been developed for a planar engagement model, with randomly jinking target maneuver and line-of-sight (LOS) rate measurement corrupted with glint noise. Two versions of fuzzy guidance schemes have bee
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::772fd12ed16c53034b44b9c98b4da4b9
https://doi.org/10.2514/3.21368
https://doi.org/10.2514/3.21368
Publikováno v:
Proceedings of National Aerospace and Electronics Conference (NAECON'94).
Two new guidance laws for short range homing missiles are developed by invoking the sliding mode control (SMC) theory. Guidance law 1 as structured around the basic proportional navigation (PN), with an additive switching term, which is a function of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e57afae412a0bfc44c18e9be037f18c
https://doi.org/10.1109/naecon.1994.332858
https://doi.org/10.1109/naecon.1994.332858
Publikováno v:
IndraStra Global.
A new approach to maneuvering target tracking using the Sliding Mode Observer theory, in the specific context of homing missile guidance, is developed. This scheme requires a priori information about the target acceleration bounds alone, and there is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a91c2b8d237bc52afa45be6ce02253df
https://igi.indrastra.com/items/show/187478
https://igi.indrastra.com/items/show/187478
Publikováno v:
Guidance, Navigation, and Control Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f08b06a0d3d55f5b4fc5b4a0aa621300
https://doi.org/10.2514/6.1994-3566
https://doi.org/10.2514/6.1994-3566
Publikováno v:
IFAC Proceedings Volumes. 15:53-56
Selftuning is applied to the control of systems whose parameters are unknown. Both linear and nonlinear systems of the Hammerstein model are considered.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d9d7c1422a308f905031b89f2d99ec0
https://doi.org/10.1016/s1474-6670(17)63324-x
https://doi.org/10.1016/s1474-6670(17)63324-x
Publikováno v:
Journal of Dynamic Systems, Measurement, and Control. 101:290-298
The specific objective of this paper is to develop multivariable controllers that would achieve asymptotic regulation in the presence of parameter variations and disturbance inputs for a tubular reactor used in ammonia synthesis. A ninth order state
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::175024451b8c91a24227c11aa18f6eb6
https://doi.org/10.1115/1.3426442
https://doi.org/10.1115/1.3426442
Publikováno v:
IEEE Transactions on Automatic Control. 25:642-651
The specific objective of this paper is to develop direct digital control strategies for an ammonia reactor using the quadratic regulator theory and compare the performance of the resultant control system with that under conventional PID regulators.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::12aa1f409ab2147f9e5d9b4a7d68fe43
https://doi.org/10.1109/tac.1980.1102447
https://doi.org/10.1109/tac.1980.1102447
Publikováno v:
Proceedings of the Indian Academy of Sciences Section C: Engineering Sciences. 1:423-440
The flight control system of a launch vehicle is the result of the right tradeoff between different objectives, such as the interaction between the control, guidance and performance aspects of a mission with specified end conditions and the analysis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c407afcaebc079f5f2316128327685fa
https://doi.org/10.1007/bf02842910
https://doi.org/10.1007/bf02842910