An Ada object oriented missile flight simulation.
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Authors
Waite, John V.
Subjects
Ada
Software Engineering
Object Oriented
Simulation
Software Engineering
Object Oriented
Simulation
Advisors
Lee, Yuh-jeng
Date of Issue
1991-09
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
This thesis uses the Ada programming language in the design and development
of an air-to-air missile flight simulation with object oriented techniques and sound
software engineering principles. The simulation is designed to be more
understandable, modifiable, efficient and reliable than earlier FORTRAN
simulations. The principles of abstraction, information hiding, modularity, high
cohesion and low coupling are used to achieve these goals. The resulting simulation
is an accurate mapping of the problem space into software. The simulation is a three
Degree-of-Freedom (3-DOF) model of RF/IR guided air-to-air missile. Two targets
are also modeled. The simulation is primarily intended to study missile kinematics.
Type
Thesis
Description
Series/Report No
Department
Computer Science
Organization
Naval Postgraduate School
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.