Author: Publisher:
ISBN:
Category : Airplanes, Military
Languages : en
Pages : 52
Book Description
Mech
Author: Technical Information Indexes
Author: United States. Naval Air Systems CommandPublisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 148
Book Description
Airplane Flying Handbook, Faa-H-8083-3b ( Full Version )
Author: Federal Aviation AdministrationPublisher: Createspace Independent Publishing Platform
ISBN: 9781719061513
Category :
Languages : en
Pages : 348
Book Description
Airplane Flying Handbook Front Matter Table of Contents Chapter 1: Introduction to Flight Training Chapter 2: Ground Operations Chapter 3: Basic Flight Maneuvers Chapter 4: Maintaining Aircraft Control: Upset Prevention and Recovery Training (PDF) Chapter 5: Takeoffs and Departure Climbs Chapter 6: Ground Reference Maneuvers Chapter 7: Airport Traffic Patterns Chapter 8: Approaches and Landings Chapter 9: Performance Maneuvers Chapter 10: Night Operations Chapter 11: Transition to Complex Airplanes Chapter 12: Transition to Multiengine Airplanes Chapter 13: Transition to Tailwheel Airplanes Chapter 14: Transition to Turbopropeller-Powered Airplanes Chapter 15: Transition to Jet-Powered Airplanes Chapter 16: Transition to Light Sport Airplanes (LSA) Chapter 17: Emergency Procedures Glossary Index
Technical Abstract Bulletin
Author: Scientific and Technical Aerospace Reports
Author: Flight Test System Identification
Author: Roger LarssonPublisher: Linköping University Electronic Press
ISBN: 9176850706
Category : Science
Languages : en
Pages : 326
Book Description
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteristics to gain flight performance, more focus has been put on model-based system engineering to help with the design work. The flight control system design is one important part that relies on this modeling. Therefore, it has become more important to develop flight mechanical models that are highly accurate in the whole flight envelope. For today’s modern fighter aircraft, the basic flight mechanical characteristics change between linear and nonlinear as well as stable and unstable as an effect of the desired capability of advanced maneuvering at subsonic, transonic and supersonic speeds. This thesis combines the subject of system identification, which is the art of building mathematical models of dynamical systems based on measurements, with aeronautical engineering in order to find methods for identifying flight mechanical characteristics. Here, some challenging aeronautical identification problems, estimating model parameters from flight-testing, are treated. Two aspects are considered. The first is online identification during flight-testing with the intent to aid the engineers in the analysis process when looking at the flight mechanical characteristics. This will also ensure that enough information is available in the resulting test data for post-flight analysis. Here, a frequency domain method is used. An existing method has been developed further by including an Instrumental Variable approach to take care of noisy data including atmospheric turbulence and by a sensor-fusion step to handle varying excitation during an experiment. The method treats linear systems that can be both stable and unstable working under feedback control. An experiment has been performed on a radio-controlled demonstrator aircraft. For this, multisine input signals have been designed and the results show that it is possible to perform more time-efficient flight-testing compared with standard input signals. The other aspect is post-flight identification of nonlinear characteristics. Here the properties of a parameterized observer approach, using a prediction-error method, are investigated. This approach is compared with four other methods for some test cases. It is shown that this parameterized observer approach is the most robust one with respect to noise disturbances and initial offsets. Another attractive property is that no user parameters have to be tuned by the engineers in order to get the best performance. All methods in this thesis have been validated on simulated data where the system is known, and have also been tested on real flight test data. Both of the investigated approaches show promising results.
The Naval Aviation Maintenance Program (NAMP).: Maintenance data systems
Author: United States. Office of the Chief of Naval OperationsPublisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 870
Book Description
Air Force Manual
Author: United States. Department of the Air ForcePublisher:
ISBN:
Category :
Languages : en
Pages : 524
Book Description
Books in Series
Author: Publisher:
ISBN:
Category : Monographic series
Languages : en
Pages : 1858
Book Description
Vols. for 1980- issued in three parts: Series, Authors, and Titles.
Defense Integrated Data System
Author: United States. Dept. of DefensePublisher:
ISBN:
Category : Database searching
Languages : en
Pages : 684
Book Description