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Showing 1 to 20 of 37 for “"Fighter Aircraft"”.

  1. Fighter Aircraft Synthesis/Design Optimization

    … subsystem-aerodynamics (AFS-A)) air-to-air fighter (AAF) with two types of AFS-A models: a fixed-wing AFS-A and a morphing-wing AFS-A. The AAF flies 19 mission segments of a supersonic fighter aircraft mission and the results of the study show that for very large structural weight penalties …

    vt Repository record for Fighter Aircraft Synthesis/Design Optimization (opens in a new tab)

  2. Optimal scheduling of fighter aircraft maintenance

    The effective scheduling of fighter aircraft maintenance in the Air Force is crucial to overall mission accomplishment. An effective maintenance scheduling policy maximizes the use of maintenance resources and aircraft availability. Currently, maintenance scheduling is a time consuming process that …

    mit Repository record for Optimal scheduling of fighter aircraft maintenance (opens in a new tab)

  3. Bifurcation analysis and control of a fighter aircraft

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.

    mit Repository record for Bifurcation analysis and control of a fighter aircraft (opens in a new tab)

  4. Structural Identification and Buffet Alleviation of Twin-Tailed Fighter Aircraft

    … dynamics of the twin tails of the F-15 fighter plane. The objective is to first investigate and identify the different possible attractors that coexist for the same operating parameters. Second is to develop a model that simulates the experimentally determined dynamics. Third is to …

    vt Repository record for Structural Identification and Buffet Alleviation of Twin-Tailed Fighter Aircraft (opens in a new tab)

  5. High performance multivariable control of the "supermaneuverable" F18/HARV fighter aircraft

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.

    mit Repository record for High performance multivariable control of the "supermaneuverable" F18/HARV fighter aircraft (opens in a new tab)

  6. Helmet-mounted display symbology for ground collision avoidance in fighter aircraft

    … Ground Collision Avoidance Systems (GCAS) for fighter aircraft through the use of Helmet-Mounted Display (HMD) symbology. Modality and information presentation issues were addressed through the design and testing of five display formats. An audio alert with no visual symbology was used as a …

    mit Repository record for Helmet-mounted display symbology for ground collision avoidance in fighter aircraft (opens in a new tab)

  7. Correlation of fighter aircraft performance with combat effectiveness in a tactically significant environment

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.

    mit Repository record for Correlation of fighter aircraft performance with combat effectiveness in a tactically significant environment (opens in a new tab)

  8. Designing for reliability, maintainability, and sustainability (RM&S) in military jet fighter aircraft engines

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.

    mit Repository record for Designing for reliability, maintainability, and sustainability (RM&S) in military jet fighter aircraft engines (opens in a new tab)

  9. A Study of Morphing Wing Effectiveness in Fighter Aircraft using Exergy Analysis and Global Optimization Techniques

    … the integrated synthesis/design of an Air-to-Air Fighter (AAF) aircraft with and without wing-morphing capability. In particular, a morphing-wing AAF is compared to a traditional fixed-wing AAF by applying large-scale optimization using exergy- and energy-based objective functions to the …

    vt Repository record for A Study of Morphing Wing Effectiveness in Fighter Aircraft using Exergy Analysis and Global Optimization Techniques (opens in a new tab)

  10. Fast half-loop maneuvers for the F/A-18 fighter aircraft using a singular perturbation feedback control law

    … nonlinear feedback control law for the F / A-I8 fighter aircraft that performs a fast half-loop maneuver. This feedback law is developed using a singular perturbation approach. A secondary purpose of this study is to establish a baseline for time optimal half-loop maneuvers. The singular …

    vt Repository record for Fast half-loop maneuvers for the F/A-18 fighter aircraft using a singular perturbation feedback control law (opens in a new tab)

  11. Applications of the Technology Acceptance Model to Integration of the Automatic Ground Collision Avoidance System in Fighter Aircraft Operations

    <p>The leading cause of F-16 fighter aircraft and fighter pilot losses is ground collisions. In an effort to curb this hazard, an automatic ground collision avoidance system (AGCAS) was formally fielded for use in routine U.S. Air Force active-duty F-16 operations in 2014. AGCAS uses a high-level …

    embry-riddle Repository record for Applications of the Technology Acceptance Model to Integration of the Automatic Ground Collision Avoidance System in Fighter Aircraft Operations (opens in a new tab)

  12. A Decomposition Strategy Based on Thermoeconomic Isolation Applied to the Optimal Synthesis/Design and Operation of an Advanced Fighter Aircraft System

    … operational optimization of an advanced tactical fighter aircraft is the focus of this research. Conceptual, time, and physical decomposition were used to solve the system-level as well as unit-level optimization problems. The total system was decomposed into five sub-systems as follows: …

    vt Repository record for A Decomposition Strategy Based on Thermoeconomic Isolation Applied to the Optimal Synthesis/Design and Operation of an Advanced Fighter Aircraft System (opens in a new tab)

  13. United States Air Force fighter jet maintenance Models : effectiveness of index policies

    … complex systems in the world, United States fighter aircraft require a complex logistics system to sustain their reliable operation and ensure that the day-to-day Air Force missions can be satisfied. While there has been a lot of attention among academics and practitioners regarding the study …

    mit Repository record for United States Air Force fighter jet maintenance Models : effectiveness of index policies (opens in a new tab)

  14. A Decision Support Model for Large Systems Using Quality Function Deployment and Goal Programming: A Capital Budgeting Problem

    … planning for the modernization of U.S. Air Force fighter aircraft requires a perception of the future tasks these aircraft will be called upon to perform, and the improvements and modifications that will be required to successfully accomplish those tasks. A great deal of research has been done in …

    odu Repository record for A Decision Support Model for Large Systems Using Quality Function Deployment and Goal Programming: A Capital Budgeting Problem (opens in a new tab)

  15. Adaptive Control of Nonaffine Systems with Applications to Flight Control

    … other aggressive flight regimes (required for fighter aircraft for example), the dynamic nonlinearities are dependent not only on the states of the system, but also on the control inputs. Hence, the conventional linearization-based logic cannot be straightforwardly extended to these flight …

    vt Repository record for Adaptive Control of Nonaffine Systems with Applications to Flight Control (opens in a new tab)

  16. Aircraft departure resistance prediction using structured singular values

    … years to determine the dynamic behavior of aircraft in unusual flight attitudes, particularly at very high angle-of-attack or post-stall conditions. The possibility that future advanced fighter aircraft will have the ability to perform controlled maneuvers at such attitudes is indicated by …

    vt Repository record for Aircraft departure resistance prediction using structured singular values (opens in a new tab)

  17. THERMODYNAMIC AND TRANSPORT PROPERTIES OF AVIATION TURBINE FUEL: PREDICTIVE APPROACHES USING ENTROPY SCALING GUIDED MACHINE LEARNING WITH EXPERIMENTAL VALIDATION

    … heat rejection, and finite heat sink capacity, fighter aircraft face significant thermal management challenges which are driving research from component to system level technology regimes. As aviation turbine fuel often represents half of the take-off weight of aircraft, it is an integral piece …

    maryland Repository record for THERMODYNAMIC AND TRANSPORT PROPERTIES OF AVIATION TURBINE FUEL: PREDICTIVE APPROACHES USING ENTROPY SCALING GUIDED MACHINE LEARNING WITH EXPERIMENTAL VALIDATION (opens in a new tab)

  18. The Impact of Birthdate Biorhythms on Aviation Accidents Involving Hellenic Air Force Fighter Pilots

    … aviation accidents involving Hellenic Air Force fighter pilots. A list of names, birthdates, and the dates of accidents was compiled from accidents involving pilots who had flown fighter aircraft and have reacted improperly even though they had sufficient time to implement the proper procedures. …

    embry-riddle Repository record for The Impact of Birthdate Biorhythms on Aviation Accidents Involving Hellenic Air Force Fighter Pilots (opens in a new tab)

  19. Reduction of a Radar Cross Section Using Active Antenna Elements

    … to RCS reduction are the Lockheed-Martin F-117 fighter aircraft, the Boeing B-2 nuclear bomber and the USS Zumwalt (DDG-1000). Here a new approach to solving this problem is explored, which is based on the principal of destructive interface between the reflected (returned) radar signal from the …

    houston Repository record for Reduction of a Radar Cross Section Using Active Antenna Elements (opens in a new tab)

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