• Refine Query
  • Source
  • Publication year
  • to
  • Language
  • 119
  • 32
  • 8
  • 7
  • 4
  • 3
  • 3
  • 1
  • 1
  • Tagged with
  • 266
  • 266
  • 105
  • 95
  • 58
  • 45
  • 35
  • 32
  • 30
  • 29
  • 24
  • 23
  • 21
  • 21
  • 21
  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
51

Control law design and validation for a helicopter in-flight simulator a thesis /

Fujizawa, Brian T. Mehiel, Eric A. January 1900 (has links)
Thesis (M.S.)--California Polytechnic State University, 2010. / Mode of access: Internet. Title from PDF title page; viewed on March 15, 2010. Major professor: Dr. Eric A. Mehiel. "Presented to the faculty of California Polytechnic State University, San Luis Obispo." "In partial fulfillment of the requirements for the degree [of] Master of Science in Aerospace Engineering." "February 2010." Includes bibliographical references (p. 80-83).
52

Aircraft simulation and robust flight control system design

Aslin, P. P. January 1985 (has links)
No description available.
53

Qualitative simulation: A tool for global decision making

Vesanterä, Pentti Juhani, 1955- January 1988 (has links)
As a decision making aid for the human operator of a highly automated, complex system, qualitative modeling is presented as a tool to mimic the human global assessment process by learning from the system behavior. Such qualitative model is applied to reason about the behavior of a quantitatively simulated aircraft model, to determine on-line when a malfunction occurs in the quantitative model, to hypothesize about the nature of this malfunction, and to suggest a global strategy that would allow to operate (control) the quantitative aircraft under the modified flying conditions. Such an algorithm could be utilized as an addition to a conventional autopilot which would allow it to remain operational after a malfunction has taken place.
54

Noninteracting control synthesis applied to a basic automatic pilot system

Rigby, Norman Carl, 1933- January 1960 (has links)
No description available.
55

Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft

Patil, Mayuresh J. 05 1900 (has links)
No description available.
56

Nonlinear flight control using neural networks

Kim, Byoung Soo 12 1900 (has links)
No description available.
57

An aeroelastic model structure investigation for a manned real-time rotorcraft simulation

Lewis, William D. 08 1900 (has links)
No description available.
58

Combined model- and rule-based controller synthesis with application to helicopter flight control

Jiang, Tian-Yue 12 1900 (has links)
No description available.
59

Fault tolerant strategies for digital aircraft control systems

Harwood, D. J. January 1984 (has links)
No description available.
60

Engineering a miniature remotely piloted helicopter

Farhat, M. A. January 1986 (has links)
No description available.

Page generated in 0.0367 seconds