Title:          Derivation of a Point-Mass Aircraft Model used for Fast-Time Simulation
Keywords:       Air Traffic Management; Avionics; Modeling and Simulation; point-mass aircraft model; fast time simulation; closed-loop aircraft model; Flight-deck Interval Management avionics; FIM avionics; aircraft guidance control laws; aircraft dynamics; aircraft control
Author:         Weitz
Creator:        LaTeX with hyperref package
Producer:       pdfTeX-1.40.14
CreationDate:   Thu Jun 25 09:56:20 2015
ModDate:        Fri Jun 26 16:20:37 2015
Tagged:         no
Form:           none
Pages:          33
Encrypted:      AES 128-bit
Permissions:    print:yes copy:yes change:no addNotes:no
Page size:      612 x 792 pts (letter) (rotated 0 degrees)
File size:      685793 bytes
Optimized:      yes
PDF version:    1.6