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DASMAT: Delft University Aircraft Simulation Model and Analysis Tool. A Matlab/Simulink Environment for Flight Dynamics and Control Analysis.

PB97185326

Publication Date	1996
Personal Author	van der Linden, C. A. A. M.
Page Count	228
Abstract	This report documents the CAD environment DASMAT, which stands for Delft University Aircraft Simulation Model and Analysis Tool. It operates in the computing environment MATLAB/SIMULINK, having high-performance numeric computation and visualization functionalities. The essential element in the DASMAT package is a generic nonlinear simulation model conceived with well-defined and generalized interfaces. For analyzing flight test data, the package also includes identification routines of which results are easily implemented in the simulation model. After a short introduction of DASMAT, this report focuses on the models, signals, and variables present in the DASMAT package. The operational aspects for the simulation and analysis tools are discussed next, followed by the application of the DASMAT package for control design purposes. The appendices include a complete list of files of the DASMAT package, the complete lists of signal formats and all essential variables used in the generic models, and the lay-out plus equations of the SIMULINK models.
Keywords	Aircraft design Computer-aided design Aircraft models Automatic flight control Aircraft control Control systems design Flight management systems Flight instruments Nonlinear systems Formats Variables Software tools Scientific visualization Computerized simulation Foreign technology DASMAT computer program DASMAT(Delft University Aircraft Simulation Model and Analysis Tool)
Source Agency	Netherlands Participating Organizations
NTIS Subject Category	51C - Aircraft 51E - Avionics 41A - Computer Aided Design, CAD 41N - Computer Software
Corporate Authors	Technische Univ. Delft (Netherlands). Faculty of Aerospace Engineering.
Supplemental Notes	Figures in this document may not be legible in microfiche. Also pub. as Technische Univ. Delft (Netherlands). Faculty of Aerospace Engineering rept. no. LR-781.
Document Type	Technical Report
NTIS Issue Number	199721

DASMAT: Delft University Aircraft Simulation Model and Analysis Tool. A Matlab/Simulink Environment for Flight Dynamics and Control Analysis.

DASMAT: Delft University Aircraft Simulation Model and Analysis Tool. A Matlab/Simulink Environment for Flight Dynamics and Control Analysis.
PB97185326

Publication Date	1996
Personal Author	van der Linden, C. A. A. M.
Page Count	228
Abstract	This report documents the CAD environment DASMAT, which stands for Delft University Aircraft Simulation Model and Analysis Tool. It operates in the computing environment MATLAB/SIMULINK, having high-performance numeric computation and visualization functionalities. The essential element in the DASMAT package is a generic nonlinear simulation model conceived with well-defined and generalized interfaces. For analyzing flight test data, the package also includes identification routines of which results are easily implemented in the simulation model. After a short introduction of DASMAT, this report focuses on the models, signals, and variables present in the DASMAT package. The operational aspects for the simulation and analysis tools are discussed next, followed by the application of the DASMAT package for control design purposes. The appendices include a complete list of files of the DASMAT package, the complete lists of signal formats and all essential variables used in the generic models, and the lay-out plus equations of the SIMULINK models.
Keywords	Aircraft design Computer-aided design Aircraft models Automatic flight control Aircraft control Control systems design Flight management systems Flight instruments Nonlinear systems Formats Variables Software tools Scientific visualization Computerized simulation Foreign technology DASMAT computer program DASMAT(Delft University Aircraft Simulation Model and Analysis Tool)
Source Agency	Netherlands Participating Organizations
NTIS Subject Category	51C - Aircraft 51E - Avionics 41A - Computer Aided Design, CAD 41N - Computer Software
Corporate Authors	Technische Univ. Delft (Netherlands). Faculty of Aerospace Engineering.
Supplemental Notes	Figures in this document may not be legible in microfiche. Also pub. as Technische Univ. Delft (Netherlands). Faculty of Aerospace Engineering rept. no. LR-781.
Document Type	Technical Report
NTIS Issue Number	199721