Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Norman Hopfe"'
Autor:
Karl W. Naumann, Norman Hopfe
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aacc3db416e16dd8005118e66e5ab0d7
https://doi.org/10.2514/6.2019-3879
https://doi.org/10.2514/6.2019-3879
Publikováno v:
SIAM Journal on Control and Optimization. 51:965-995
Tracking of reference signals $y_{\mathrm{ref}}(\cdot)$ by the output $y(\cdot)$ of linear (as well as a considerably large class of nonlinear) single-input, single-output systems is considered. The system is assumed to have strict relative degree tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43ee08871a4002c5d9180ffd363fa60a
https://doi.org/10.1137/100799903
https://doi.org/10.1137/100799903
Publikováno v:
IFAC Proceedings Volumes. 46:125-130
A Throttleable Ducted Rocket (TDR) is a ramjet-type engine using a solid propellant for which the fuel mass flow rate can be controlled. Since the propellant has an oxygen deficient formulation, fuel rich combustion products are produced within the g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d4692185ec7a0fbd7d9b8b72412f8d7
https://doi.org/10.3182/20130902-5-de-2040.00084
https://doi.org/10.3182/20130902-5-de-2040.00084
Publikováno v:
IEEE Transactions on Automatic Control. 55:2177-2182
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e92f2112ad4112b9a6e4ffe88a85657
https://doi.org/10.1109/tac.2010.2051735
https://doi.org/10.1109/tac.2010.2051735
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
This paper comprises the methodology applied for the performance assessment of a throttleable ducted rocket (TDR) powered lower tier interceptor achieving average flight Mach numbers in the vicinity of M > 5. Contrary to conventional ground-to-air sy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d37d0aea8e7812f9c61611203a976c07
https://doi.org/10.2514/6.2015-4234
https://doi.org/10.2514/6.2015-4234
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A Throttleable Ducted Rocket (TDR) is a ramjet-type engine using a solid propellant for which the fuel mass flow rate can be controlled. Since the propellant has an oxygen deficient formulation, fuel rich combustion products are produced within the g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d97bfa2ddaba8b0df72ef042d4c3ee6
https://doi.org/10.2514/6.2012-3827
https://doi.org/10.2514/6.2012-3827
Publikováno v:
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
formulation which produces fuel rich combustion products within the gas generator, which will be exhausted into the ram combustor. There, these products will be further combusted with the incoming air provided by the air intakes (AI). For a TDR it is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12aa4a617e45b789326f922bc94f3c83
https://doi.org/10.2514/6.2011-5610
https://doi.org/10.2514/6.2011-5610
Publikováno v:
Hopfe, N, Ilchmann, A & Ryan, E P 2010, ' Funnel control with saturation: Linear MIMO systems ', IEEE Transactions on Automatic Control, vol. 55, no. 2, pp. 532-538 . https://doi.org/10.1109/tac.2009.2037475
Tracking-by the system output-of a reference signal (assumed bounded with essentially bounded derivative) is considered in the context of a class of nonlinear, single-input, single-output systems modelled by functional differential equations and subj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8012ca428ae520b5ec127269d55205f6
https://purehost.bath.ac.uk/ws/files/304556/hopfe-55-2.pdf
https://purehost.bath.ac.uk/ws/files/304556/hopfe-55-2.pdf
