• No results found

aircraft flight

On the development of computer code for aircraft flight dynamics analysis

On the development of computer code for aircraft flight dynamics analysis

... developing flight simulator, one to follow certain steps, one have to be able to evaluate the aircraft behavior in linear as well as in nonlinear of the aircraft flight of ...equation‟s ...

36

Aircraft Flight Control Simulation Using Parallel Cascade Control

Aircraft Flight Control Simulation Using Parallel Cascade Control

... Abstract Aircraft flight simulation is a billion dollar industry worldwide that requires vast engineering ...modeling flight control systems using parallel cascade system identification is proposed ...

9

Evolution of Aircraft Flight Control System and Fly-By-Light Flight Control System

Evolution of Aircraft Flight Control System and Fly-By-Light Flight Control System

... Aircraft flight control was traditionally accomplished through mechanical & hydraulic ...in aircraft offers considerable advantages for flight control ...in aircraft which provides ...

5

Experiments on aircraft flight parameter detection by on skin sensors

Experiments on aircraft flight parameter detection by on skin sensors

... Modern aircrafts require a vast amount of data coming from on board sensors, either to provide information to the pilot, to implement Fly-by-Wire (FBW) systems, or to achieve automatic flight control as in ...

11

Variable Cant Angle Winglets for Improvement of Aircraft Flight Performance

Variable Cant Angle Winglets for Improvement of Aircraft Flight Performance

... improving aircraft performance and fuel e ffi ...erent flight conditions (take-o ff , climb, cruise, loitering, descent, approach, landing, and so ...allow aircraft to get the best all-around ...

32

Predictive Modeling of Aircraft Flight Delay

Predictive Modeling of Aircraft Flight Delay

... There have been predictive modeling and simulation attempts to forecast delay in advance. Juan Jose Rebollo and Hamsa Balakrishnan [4] summarized the results of different classification and regression models based on 100 ...

7

Two-Aircraft optimal control problem. The in-flight noise reduction*,, **

Two-Aircraft optimal control problem. The in-flight noise reduction*,, **

... the aircraft trajectory resulting from the two trajectories ...two-aircraft flight-angles and throttles evolution versus time as recom- mended by ICAO during aircraft ...the aircraft ...

7

Aircraft Type Identification Using Reinforcement Active Learning

Aircraft Type Identification Using Reinforcement Active Learning

... In each episode, 30 aircraft flight tracks were randomly selected from 3 randomly sampled classes, without replacement. Here, the number of samples from each class may not be balanced. Each selected class ...

7

The Construction of an Ontology Based Knowledge Management Model for Departure Procedures

The Construction of an Ontology Based Knowledge Management Model for Departure Procedures

... guide aircraft to ac- complish flight operations safely and efficiently using information provided by radar such as height, speed, weather and relevant aviation ...between aircraft and knowing the ...

17

Volume 1, Issue 2 (2015)

Volume 1, Issue 2 (2015)

... to flight safety requirements”. As explained in the final report, flight crews’ working hours at different times of day are very often different from those commonly acknowledged as most favorable from the ...

16

Developing a Feedback System to Augment Pilots Monitoring Performance

Developing a Feedback System to Augment Pilots Monitoring Performance

... each flight phase-information source pair a relevance value and a maximum neglect time in ...each flight phase from “not relevant” to “very relevant”, and from “low maximum neglect” time to “high maximum ...

7

Information support of reconfigurable flight control system of the aircraft

Information support of reconfigurable flight control system of the aircraft

... the aircraft exterior contour and the assessment of the impact of the quality of oil on the operation of the engine in conditions of aircraft’s reconfiguration control with a damaged tail have been ...of ...

6

remote pilot study guide 16

remote pilot study guide 16

... the flight: Pilot, Aircraft, enVironment, and External pressures, which makes up the PAVE ...any flight. Pay special attention to the pilot-aircraft combination, and consider whether the ...

87

Development and Flight Test of a Multi-Function Controller for Automated Cruise Flaps on an Aircraft Wing

Development and Flight Test of a Multi-Function Controller for Automated Cruise Flaps on an Aircraft Wing

... an aircraft with an automated cruise flap which was controlled using the instantaneous coefficient of lift as the sole ...Although aircraft such as uninhabited air vehicles (UAVs) are probably equipped with ...

169

The development of a fixed wing aircraft analysis and design flight dynamic software

The development of a fixed wing aircraft analysis and design flight dynamic software

... the flight control system of an aircraft FCS generally consists of three important ...the aircraft. This is done by using the control surfaces to make the aircraft more ...the aircraft ...

58

Different Automation Concepts in Civil Aircraft Cockpits of Today and Their Influence on Airline Flight Operations

Different Automation Concepts in Civil Aircraft Cockpits of Today and Their Influence on Airline Flight Operations

... New technology has always introduced chal- lenges and potential operational difficulties. They lead to the emergence of new science dealing with human factors related to the interaction of pilots and advanced system in ...

6

Onboard Flight Safety Support System Development for Low-Altitude Flights of Light Aircraft

Onboard Flight Safety Support System Development for Low-Altitude Flights of Light Aircraft

... particular, FV, the essential feature is the need to operate in real time using the onboard computer equipment. These features impose strict requirements both to the actual algorithms of data collection and processing ...

8

Models and the scaling of energy costs for locomotion

Models and the scaling of energy costs for locomotion

... My interest here is in widely applicable scaling rules; for example in rules that will predict the scaling of running over the range from small rodents to elephants, or of flight from sparrows to swans. Mice are ...

8

Evaluating GNSS integrity augmentation techniques for UAS sense and avoid

Evaluating GNSS integrity augmentation techniques for UAS sense and avoid

...  When the multipath ranging error exceeds 2 metres and the aircraft flies in proximity of the ground (below 500 ft AGL), the warning integrity flag shall be generated. In order to define the integrity thresholds ...

8

The impact of altitude, latitude, and endurance duration on the design of a high altitude, solar powered unmanned aerial vehicle

The impact of altitude, latitude, and endurance duration on the design of a high altitude, solar powered unmanned aerial vehicle

... Sustained flight at high altitudes involves a range of challenges such as low air density which can cause problems in generating sufficient lift and ...thrust. Aircraft speed can be adjusted but the ...

7

Show all 3500 documents...

Related subjects