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Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Appendix I / Utilities<br />

_ _<br />

22.1 Utility CMS Groups<br />

22.1.1 General Utilities<br />

CMS group [ GENERAL ]<br />

General utilities comprise 23 system clocks ranging from 1Hz to 8kHz split<br />

from a 16 kHz Master Clock; Runge-Kutta state integration (order 1-4);<br />

function gradients; random number generators (Normal, Uniform, Rayleigh<br />

and Bi-normal); statistical analysis package used by the interactive interface;<br />

function and surface interpolation modules.<br />

System Clock Update<br />

Runge-Kutta Integration<br />

Real Variable Comparator<br />

Random Number Generator<br />

PRBS Initialisation<br />

Normal Distributed Variables<br />

Bi-modally Distributed Variables<br />

Uniformly Distributed Variables<br />

Rayleigh Distributed Variables<br />

Simulation PRBS Noise Sequences<br />

22.1.2 WGS 84, Target and Missile Data<br />

CMS group [ GEOMETRY ]<br />

22.1-3<br />

Time and Date Stamp<br />

Recursive Statistical Analyser<br />

Integer Word Bit Manipulation<br />

1D Linear Interpolation<br />

2D Bi-Linear Interpolation<br />

Numerical Differentiation<br />

ASCII to Integer Re-formatting<br />

Convex Surface Testing<br />

Integer Word Single Bit Delay<br />

Simulation speed has been sacrificed to provide commonly used point-mass<br />

kinematics. This information is refreshed at a rate in excess of any practical<br />

system implementation so as to promote rapid algorithm development. The<br />

data is derived from the reference states and, where possible, from state<br />

observer output. The simulation variables relating to this data have been<br />

selected as prescribed in the Glossary with those derived from the observer<br />

states prefixed by”F_”.<br />

Closest Approach Detection and Reporting<br />

Geodetic Referenced Parameters<br />

Target Kinematics<br />

22.1.3 Axis Transformations<br />

CMS group [ AXTRAN ]<br />

Missile Kinematics<br />

Missile/Target Relative Inertial Kinematics<br />

Relative Missile and Target Kinematics<br />

These utilities deal with the conversion between Cartesian and Polar coordinates,<br />

and transformation matrix direction cosines. They cover the<br />

projection of vectors onto the principal planes of a frame, and the angle<br />

subtended by the rotation of one frame with respect to another.

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