A Nonlinear Six Degree Of Freedom Ballistic Aerial Target Simulation Model Volume 1 Theoretical Development
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Total Pages | : 51 |
Release | : 1984 |
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Six degree-of-freedom, rigid body equations of motion are described suitable for modeling the dynamic characteristics of multistaged, free-flight, ballistic rockets such as the DRES developed aerial targets CRV7/BATS and ROBOT- 9. These equations of motion form the core of a FORTRAN simulation software package called BALSIM. This package allows for modeling of vehicle thrust and structural symmetries, time-varying mass and inertia characteristics, variable wind conditions, nonstandard atmospheric conditions, stage failures, and different rocket motor types. The BALSIM package has been written in IBM FORTRAN IV and has been tested on the IBM 3033 computer with the H-extended compiler. It is currently being adapted for use with the VAX11/780 and Honeywell DPS-8/70C computers.
Author | : A. B. Markov |
Publisher | : |
Total Pages | : 94 |
Release | : 1983 |
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Six degree-of-freedom, rigid body equations of motion are described suitable for modeling the dynamic characteristics of multistaged, free-flight, ballistic rockets such as the DRES developed aerial targets CRV7/BATS and ROBOT-9. These equations of motion form the core of a FORTRAN simulation software package called BALSIM. This package allows for modeling of vehicle thrust and structural asymmetries, time-varying mass and inertia characteristics, variable wind conditions, nonstandard atmospheric conditions, stage failures, and different rocket motor types. The BALSIM package has been written in IBM FORTRAN IV and has been tested on the IBM 3033 computer with the H-extended compiler. It is currently being adapted for use with the VAX11/780 and Honeywell DPS-8/70C computers. (Author).
Author | : A. B. Markov |
Publisher | : |
Total Pages | : 0 |
Release | : 1990 |
Genre | : Cruise missiles |
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"Six degree-of-freedom, rigid body equations of motion are described suitable for modeling the dynamic characteristics of multistaged rocket-boosted maneuvering aerial targets such as the DRES developed ROBOT-X. These equations of motion form the core of a Fortran simulation package called FLISIM. FLISIM is currently installed on a VAX 11/780 computer and allows for modeling of vehicle thrust and structural asymmetries, time-varying mass and inertia characteristics, autopilot control laws, autopilot update rates, autopilot sensor non-idealities, nonlinear aerodynamic characteristics, variable wind conditions, turbulence, nonstandard atmospheric conditions, stage and individual motor failures, different rocket motor types, and parachute deceleration dynamics. The FLISIM software package has been developed in two versions (FLISIMV1 and FLISIMV2) using two different aerodynamic models. Both are written in VAX 11 Fortran and run under the VMS Operating System. FLISIM is fully supported with a plotting software package (PLTSIM) developed around Tektronix PLOT 10 core software"--abstract.
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Total Pages | : 1264 |
Release | : 1984-10 |
Genre | : Science |
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Author | : |
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Total Pages | : 1528 |
Release | : 1984 |
Genre | : Government reports announcements & index |
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Total Pages | : 1520 |
Release | : 199? |
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ISBN | : |
Author | : Alexander B. Markov |
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Total Pages | : |
Release | : 1990 |
Genre | : |
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Author | : |
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Total Pages | : 1572 |
Release | : 1992 |
Genre | : Aeronautics |
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Total Pages | : 31 |
Release | : 1964 |
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A six degree of freedom model for digital simulation of the trajectory of an unguided, fin-stabilized rocket is developed. A derivation of the equations and an explanation of the equations and an explanation of the coordinate systems are presented. The development assumes that the trajectory will be over a rotating planet with a variable atmosphere. A space-variable, three-dimensional wind vector is assumed. The equations of motion are derived from Newton's Laws of Motion. The aerodynamic forces and moments are based on the theory of stability derivatives and the assumption of linear aerodynamics. The body axes are assumed to be principal axes of inertia.
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Total Pages | : 1048 |
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Genre | : Science |
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