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de Jong, H. (author)
Publikatie naar aanleiding van een presentatie voor de Nederlandse Vereniging voor Ruimtevaart, gehouden op 22 februari 1990. In deze publikatie wordt een overzicht gegeven van MIMOSE (Machine Independent Model Oriented Simulation Environment). MIMOSE is een ontwikkelomgeving waarmee simulatiesystemen kunnen worden samengesteld, waaronder...
report 1990
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Puthli, R.S. (author), de Jong, C.H.M. (author), Romein, A. (author), Panjeh, E. (author), Verheul, A. (author)
report 1990
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Prins, J.J.M. (author), Dieleman, P. (author), de Jong, H. (author)
The Hermes manipulation system (HERA) is a sophisticated space manipulator system, which has to perform tasks ranging from berthing to tool operation in various operational modes from fully automatic to purely manual. The HERA system main contractor is Fokker Space & Systems B.V. (FSS). Development and qualification of such a space-based...
report 1989
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Groothuizen, R.J.P. (author), ten Dam, A.A. (author), de Jong, H. (author)
Requirements are formulated for an environment for development, verification and validation of digital simulation models of multibody systems. A realization of such an environment at the National Aerospace Laboratory NLR is described.
report 1989
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van Zijderveld, E.J.A. (author), de Jong, J. (author)
report 1989
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Pronk, C.N.A. (author), de Jong, H. (author), Lippay, A.L. (author), Ersü, E. (author)
report 1987
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Dekker, G.J. (author), de Jong, H. (author), Moek, G. (author)
Under contract to ESA, NLR has developed a flexible simulation package, named PROMISE, and a set of simulation models of the ESA proposed NAVSAT satellite-based navigation system. These were completed in 1984. In a continuation contract, described in this report, a number of extensions have been developed and implemented, and a number of...
report 1987
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Dekker, G.J. (author), de Jong, H. (author), Moek, G. (author)
report 1987
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de Jong, Th. (author)
report 1987
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de Jong, H. (author), Becqué, R.F. (author)
report 1986
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de Jong, J.B. (author), van Lummel, C.W.J. (author)
A method is developed to quantify the severity of recorded stress spectra in terms of potential crack growth. The CSI (Crack Severity Index) defined is Intended for application to the stress monitoring results obtained in RNLAF F-16 aircraft. However, the methodology can be used for other applications, associated with other types of stress spectra.
report 1986
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de Jong, R.P.M. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, R.P.M. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, L.P. (author)
report 1986
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de Jong, H. (author)
report 1985
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