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Aircraft used for the evaluation

Evaluation of remotely piloted aircraft in surveying applications

Evaluation of remotely piloted aircraft in surveying applications

... Figure 3.7: Displaying an error in orientation. Notice scan position 1 and 2 appear to line-up, however scan position 3 appears to be disoriented. 3 - Post-processing It is essential to “clean” the data prior to ...

247

A model for aircraft evaluation to support strategic decisions

A model for aircraft evaluation to support strategic decisions

... best aircraft among a set of alternatives. Authors used the method of the hypothetical equivalents and inequivalents (Wu, 1996), basing their choice on three criteria: speed, range and number of ...of ...

18

The brace position for passenger aircraft: a biomechanical evaluation

The brace position for passenger aircraft: a biomechanical evaluation

... be used for personal research or study, educational, or not- for-profit purposes without prior permission or charge provided that the authors, title and full bibliographic details are credited, a hyperlink and/or ...

353

High-resolution evaluation of aircraft emissions at airports

High-resolution evaluation of aircraft emissions at airports

... and aircraft fleet compositions at major international airports such as London Heathrow airport, which was adopted as the case ...be used to ensure that the current confidence limits are applicable for ...

242

Evaluation of paralleled generation architectures for civil aircraft applications

Evaluation of paralleled generation architectures for civil aircraft applications

... Voltage-behind-impedance models with representative dc side capacitive filters are employed to represent the converter interfaced wound field generation systems in an averaged-value manner. These models accurately ...

8

Design and Evaluation of Nextgen Aircraft Separation Assurance Concepts

Design and Evaluation of Nextgen Aircraft Separation Assurance Concepts

... and evaluation of allocating separation assurance responsibilities and workload to these three ...simulation used to evaluate these concepts, while Sections IV and V ...

12

Evaluation of Aircraft Impact Analysis Methodologies for Nuclear Safety Applications

Evaluation of Aircraft Impact Analysis Methodologies for Nuclear Safety Applications

... the aircraft and contents were properly captured for implementation in the impact ...commercial aircraft model included all of the primary structural component throughout the wings, fuselage and ...were ...

10

Review on Fatigue and Damage Tolerance Evaluation of Aircraft Lug Joint

Review on Fatigue and Damage Tolerance Evaluation of Aircraft Lug Joint

... Liangmo Wang [3]: For the improvement of Aluminum wheel quality, new method is proposed for evaluating fatigue life. Abacus software is used for post processing operation. By the effects of mean loads, fatigue ...

5

Rapid evaluation of building and infrastructure to accidental and deliberate aircraft impact

Rapid evaluation of building and infrastructure to accidental and deliberate aircraft impact

... the aircraft structure is built based upon the aircraft drawings and material property ...C-130 aircraft are shown in ...the aircraft, wings and around the landing gear areas were included in ...

8

Evaluation of Fire Test Methods for Aircraft Thermal Acoustical Insulation

Evaluation of Fire Test Methods for Aircraft Thermal Acoustical Insulation

... Five test blankets, each measuring 16 by 24 inches, were fabricated and sent to each participant. Each blanket was constructed of fiberglass insulation encapsulated with one of the five film materials. Two different ...

23

UNMANNED AIRCRAFT COLLISION AVOIDANCE TECHNOLOGY ASSESSMENT AND EVALUATION METHODS

UNMANNED AIRCRAFT COLLISION AVOIDANCE TECHNOLOGY ASSESSMENT AND EVALUATION METHODS

... Given that it is sometimes difficult to conduct the required number of trials, simulation methods are often employed. Simulation is used to correctly model the environment, i.e., geometries that represent ...

10

Realization and Evaluation of an Aircraft Onboard Retrofit Trajectory Management System

Realization and Evaluation of an Aircraft Onboard Retrofit Trajectory Management System

... currently used RNAV ...the aircraft from the ...the aircraft was stabilized again in FL120, the pilot entered time constraints at OSN and VISKI as time windows of ten seconds ...was used only ...

207

Environmental Control System Testing and Performance Evaluation of a Transport Aircraft

Environmental Control System Testing and Performance Evaluation of a Transport Aircraft

... Dual Heat Exchanger (item 10) where the temperature is reduced to near the ambient air (used for cooling in heat exchanger) temperature. After passing through the high- pressure water separation system condenser ...

5

Modelling and evaluation of aircraft contrails for 4-dimensional trajectory optimisation

Modelling and evaluation of aircraft contrails for 4-dimensional trajectory optimisation

... restricts aircraft to cruise at discrete flight levels, the solution implemented in this article adopts a 2-Dimensional plus Time (2D+T) trajectory optimization approach at constant flight ...A320 aircraft ...

11

Evaluation of avian hazards to aircraft at Dallas/Fort Worth International Airport

Evaluation of avian hazards to aircraft at Dallas/Fort Worth International Airport

... methods used may be of little interest to some people, and the text would be interrupted by lengthy technical ...techniques used in this research are discussed in greater ...

173

Engine Company Evaluation of Feasibility of Aircraft Retrofit Water-Injected Turbomachines

Engine Company Evaluation of Feasibility of Aircraft Retrofit Water-Injected Turbomachines

... 12.0 Performance Analysis of Water Injected in Front of LPC Simulation modeling is used to evaluate the effect of water injection on engine performance. 12.1 Performance Simulation Model The PW4062A performance ...

35

Multiple Criteria Decision Analysis Techniques in Aircraft Design and Evaluation Processes

Multiple Criteria Decision Analysis Techniques in Aircraft Design and Evaluation Processes

... Over the past decades, considerable research has been conducted to deal with the selection of the most appropriate MCDA method for a given decision making problem. MacCrimmon firstly recognized the importance of MCDA ...

224

Simulation and Performance Evaluation of Algorithms for Unmanned Aircraft Conflict Detection and Resolution

Simulation and Performance Evaluation of Algorithms for Unmanned Aircraft Conflict Detection and Resolution

... Typically, sequential Monte Carlo has been used for the problem of state estimation and is generally labeled as particle filtering. Only recently has SMC been used for solving MPC optimization problems [9, ...

56

Best Management Practice for Management of Used Aircraft Parts and Assemblies and for Recycling of Aircraft Materials

Best Management Practice for Management of Used Aircraft Parts and Assemblies and for Recycling of Aircraft Materials

... when used in reference to an Asset, means to dispose of the remainder of the Asset in a permissible manner – including all parts and assemblies that are not being retained as airworthy aircraft parts ...

112

An Optimized Thermal Analysis of Electronic Unit Used in Aircraft

An Optimized Thermal Analysis of Electronic Unit Used in Aircraft

... an aircraft having suspected thermal characteristics owing to abrupt changes in pressure and temperature as aircraft moves quickly from a lower altitude to higher ...

19

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