Results 181 to 190 of about 217,272 (213)

Community Noise Reduction Using Continuous Descent Approach: A Demonstration Flight Test at Louisville

, 2003
A flight demonstration test was conducted at the Louisville International Airport (KSDF) by a research team comprised of personnel from the Boeing Company, the Federal Aviation Administration (FAA), the Massachusetts Institute of Technology (MIT), the ...
K. Elmer, Joeseph Wat, B. Shivashankara, A. Warren, K. Tong, J. Clarke   +5 more
semanticscholar   +1 more source

Detection and Classification of Faults in Aeronautical Gas Turbine Engine: a Comparison Between two Fuzzy Logic Systems

IEEE International Conference on Fuzzy Systems, 2018
Gas turbines are the most common engine used in the majority of commercial aircraft. Due to its criticality, to detect and classify faults in a gas turbine is extremely important.
M. G. C. Ribeiro, P. Calderano, R. P. F. Amaral, Ivan Fabio Mota de Menezes, R. Tanscheit, M. Vellasco, Eduardo Pestana de Aguiar   +6 more
semanticscholar   +1 more source

Advanced Noise Abatement Procedures for Approach and Departure

, 2002
Deputy Head Flight Mechanics Department NLR. Copyright © 2002 by the National Aerospace Laboratory NLR. Published by the American Institute Of Aeronautics and Astronautics, Inc. with permission.
L. Erkelens
semanticscholar   +1 more source

In-Flight Performance of the Mars Science Laboratory Spacecraft Cruise Phase Thermal Control Systems

, 2012
The National Aeronautics and Space Administration’s Mars Science Laboratory (MSL) mission will land a robotic rover on the surface of Mars for a two-year exploration mission.
A. Paris, F. Kelly, Joshua E. Kempenaar, K. Novak   +3 more
semanticscholar   +1 more source

Verification & Validation by Risk Class: Understanding how Risk Classes affect the V&V process

, 2013
There is an oft quoted saying in the space industry, “Every mission is Class A on the Launch Pad”. No matter the stated risk class of your mission, when it is time to launch, the mission must be a success.
B. Solish, B. Cooke, Nagin Cox, P. Kahn, Pavani Peddada, R. Prakash   +5 more
semanticscholar   +1 more source

Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model

Russian Aeronautics, 2018
Yu. M. Ignatkin, P. Makeev, V. I. Shaidakov, A. Shomov   +3 more
semanticscholar   +2 more sources

Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model

Russian Aeronautics, 2019
Yu. M. Ignatkin, P. Makeev, V. I. Shaidakov, A. Shomov   +3 more
semanticscholar   +1 more source

Analytical Synthesis of a Modal Controller by Output Vector for Attitude Control of a Descent Module during Its Descent in the Earth’s Atmosphere

Russian Aeronautics, 2019
N. Zubov, A. Lapin, V. Ryabchenko
semanticscholar   +1 more source

Entry, Descent, and Landing performance trades to increase landed mass for the Mars 2018 mission

IEEE Aerospace Conference, 2012
R. Winski, E. García-Llama, R. Prakash, J. Shidner, M. Grover, M. Ivanov   +5 more
semanticscholar   +1 more source

Statistical analysis for rotational motion of a light descent capsule under deployment of a space cable system

Russian Aeronautics (Iz VUZ), 2012
O. Naumov
semanticscholar   +1 more source