- 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.
Search results
Showing 1 to 10 of 30 (0.088 seconds)Spelling suggestions: "subject:"airplanes - eontrol lemsystems"" "subject:"airplanes - eontrol atemsystems""
| 1 |
An aircraft power-control optimalizing computerAngelopoulos, Panayiotis Athanassios, 1932- January 1958 (has links)
No description available.
|
| 2 |
The design and evaluation of a flight simulator apparatusKaith, Irving, 1928- January 1960 (has links)
No description available.
|
| 3 |
The effects of the direction of control loading on a one-dimensional tracking taskCarlin, James Michael 05 1900 (has links)
No description available.
|
| 4 |
Flight envelope limit detection and avoidanceHorn, Joe 05 1900 (has links)
No description available.
|
| 5 |
An agent-based cockpit task management system : a task-oriented pilot-vehicle interfaceKim, Joong Nam 17 November 1994 (has links)
Graduation date: 1995
|
| 6 |
Qualitative simulation: A tool for global decision makingVesanterä, 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.
|
| 7 |
Adaptive nonlinear flight controlRysdyk, Rolf T. 12 1900 (has links)
No description available.
|
| 8 |
On minimum time six-degree-of-freedom turning maneuvers for a high-alpha fighter aircraftHoffman, Eric 08 1900 (has links)
No description available.
|
| 9 |
An investigation of a method of aircraft control by shock wave interferenceAldridge, Edward Cleveland 12 1900 (has links)
No description available.
|
| 10 |
Aircraft cruise performance optimization using chattering controlsBhardwaj, Pradeep 15 November 2013 (has links)
Aircraft Cruise Performance is examined by using energy-state modelling to investigate fuel-range optimal trajectories. Chattering controls are considered appropriate when the hodograph is non-convex.
Classical steady-state cruise, simple chattering-cruise and the extended chattering-cruise models are studied as constrained parameter-optimization problems. The term "extended chattering" refers to vehicle system modelling extended to maintain vertical equilibrium only on the average. Numerical solution is obtained using a variable-metric gradient-protection algorithm and computational results are presented for three different aircraft.
This study shows that simple chattering cruise for certain specific energies can result in substantial fuel savings over classical steady-state cruise. However extended chattering cruise results in only marginal fuel savings when compared to simple chattering cruise. / Master of Science
|
Page generated in 0.0928 seconds