17 lines
815 B
Plaintext
17 lines
815 B
Plaintext
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Title: Derivation of a Point-Mass Aircraft Model used for Fast-Time Simulation
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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
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Author: Weitz
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Creator: LaTeX with hyperref package
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Producer: pdfTeX-1.40.14
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CreationDate: Thu Jun 25 09:56:20 2015
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ModDate: Fri Jun 26 16:20:37 2015
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Tagged: no
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Form: none
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Pages: 33
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Encrypted: AES 128-bit
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Permissions: print:yes copy:yes change:no addNotes:no
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Page size: 612 x 792 pts (letter) (rotated 0 degrees)
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File size: 685793 bytes
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Optimized: yes
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PDF version: 1.6
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