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Book Rollout and Turnoff  Roto  Guidance and Information Displays  Effect on Runway Occupancy Time in Simulated Low Visibility Landings

Download or read book Rollout and Turnoff Roto Guidance and Information Displays Effect on Runway Occupancy Time in Simulated Low Visibility Landings written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-10-03 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report examines a rollout and turnoff (ROTO) system for reducing the runway occupancy time for transport aircraft in low-visibility weather. Simulator runs were made to evaluate the system that includes a head-up display (HUD) to show the pilot a graphical overlay of the runway along with guidance and steering information to a chosen exit. Fourteen pilots (airline, corporate jet, and research pilots) collectively flew a total of 560 rollout and turnoff runs using all eight runways at Hartsfield Atlanta International Airport. The runs consisted of 280 runs for each of two runway visual ranges (RVRs) (300 and 1200 ft). For each visual range, half the runs were conducted with the HUD information and half without. For the runs conducted with the HUD information, the runway occupancy times were lower and more consistent. The effect was more pronounced as visibility decreased. For the 1200-ft visibility, the runway occupancy times were 13% lower with HUD information (46.1 versus 52.8 sec). Similarly, for the 300-ft visibility, the times were 28% lower (45.4 versus 63.0 sec). Also, for the runs with HUD information, 78% (RVR 1200) and 75% (RVR 300) had runway occupancy times less than 50 sec, versus 41 and 20%, respectively, without HUD information. Hueschen, Richard M. and Hankins, Walter W., III and Barker, L. Keith Langley Research Center NASA/TM-2001-211057, L-18084, NAS 1.15:211057

Book Rollout and Turnoff  roto  Guidance and Information Displays  Effect on Runway Occupancy Time in Simulated     Nasa

Download or read book Rollout and Turnoff roto Guidance and Information Displays Effect on Runway Occupancy Time in Simulated Nasa written by United States. National Aeronautics and Space Administration and published by . This book was released on 2003* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Guidance and Control Design for High Speed Rollout and Turnoff  Roto

Download or read book Guidance and Control Design for High Speed Rollout and Turnoff Roto written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-25 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt: A ROTO architecture, braking and steering control law and display designs for a research high speed Rollout and Turnoff (ROTO) system applicable to transport class aircraft are described herein. Minimum surface friction and FMS database requirements are also documented. The control law designs were developed with the aid of a non-real time simulation program incorporating airframe and gear dynamics as well as steering and braking guidance algorithms. An attainable objective of this ROTO system, as seen from the results of this study, is to assure that the studied aircraft can land with runway occupancy times less then 53 seconds. Runway occupancy time is measured from the time the aircraft crosses the runway threshold until its wing tip clears the near side of the runway. Turnoff ground speeds of 70 knots onto 30 degree exits are allowed with dry and wet surface conditions. Simulation time history and statistical data are documented herein. Parameters which were treated as variables in the simulation study include aircraft touchdown weight/speed/location, aircraft CG, runway friction, sensor noise and winds. After further design and development of the ROTO control system beyond the system developed earlier, aft CG MD-11 aircraft no longer require auto-asymmetric braking (steering) and fly-by-wire nose gear steering. However, the auto ROTO nose gear hysteresis must be less than 2 degrees. The 2 sigma dispersion certified for MD-11 CATIIIB is acceptable. Using this longitudinal dispersion, three ROTO exits are recommended at 3300, 4950 and 6750 feet past the runway threshold. The 3300 foot exit is required for MD-81 class aircraft. Designs documented in this report are valid for the assumptions/models used in this simulation. It is believed that the results will apply to the general class of transport aircraft; however further effort is required to validate this assumption for the general case. Goldthorpe, S. H. and Dangaran, R. D. and Dwyer, J. P. and McBee, L. S. an...

Book SENSITIVITY OF RUNWAY OCCUPANCY TIME  ROT  TO VARIOUS ROLLOUT AND TURNOFF  ROTO  FACTORS FINAL REPORT    NASA CR 1997 201712 VOL1    OCT  26

Download or read book SENSITIVITY OF RUNWAY OCCUPANCY TIME ROT TO VARIOUS ROLLOUT AND TURNOFF ROTO FACTORS FINAL REPORT NASA CR 1997 201712 VOL1 OCT 26 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1999* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book SENSITIVITY OF RUNWAY OCCUPANCY TIME  ROT  TO VARIOUS ROLLOUT AND TURNOFF  ROTO  FACTORS FINAL REPORT    NASA CR 1997 201712 VOL2    OCT  26

Download or read book SENSITIVITY OF RUNWAY OCCUPANCY TIME ROT TO VARIOUS ROLLOUT AND TURNOFF ROTO FACTORS FINAL REPORT NASA CR 1997 201712 VOL2 OCT 26 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1999* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Sensitivity of Runway Occupancy Time  ROT  to Various Rollout and Turnoff  ROTO  Factors

Download or read book Sensitivity of Runway Occupancy Time ROT to Various Rollout and Turnoff ROTO Factors written by S. H. Goldthorpe and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Langley Scientific and Technical Information Output 2001

Download or read book NASA Langley Scientific and Technical Information Output 2001 written by and published by . This book was released on 2002 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Guidance and Control Requirements for High speed Rollout and Turnoff  ROTO

Download or read book Guidance and Control Requirements for High speed Rollout and Turnoff ROTO written by and published by . This book was released on 1995 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Runway Incursion Prevention System  Rips  Dallas Fort Worth Demonstration Performance Analysis

Download or read book NASA Runway Incursion Prevention System Rips Dallas Fort Worth Demonstration Performance Analysis written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-13 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA's Aviation Safety Program Synthetic Vision System project conducted a Runway Incursion Prevention System (RIPS) flight test at the Dallas-Fort Worth International Airport in October 2000. The RIPS research system includes advanced displays, airport surveillance system, data links, positioning system, and alerting algorithms to provide pilots with enhanced situational awareness, supplemental guidance cues, a real-time display of traffic information, and warnings of runway incursions. This report describes the aircraft and ground based runway incursion alerting systems and traffic positioning systems (Automatic Dependent Surveillance - Broadcast (ADS-B) and Traffic Information Service - Broadcast (TIS-B)). A performance analysis of these systems is also presented. Cassell, Rick and Evers, Carl and Esche, Jeff and Sleep, Benjamin and Jones, Denise R. (Technical Monitor) Langley Research Center NAS1-00108; RTOP 728-60-30-01

Book Aerospace America

Download or read book Aerospace America written by and published by . This book was released on 1998 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book International Encyclopedia of Ergonomics and Human Factors   3 Volume Set

Download or read book International Encyclopedia of Ergonomics and Human Factors 3 Volume Set written by Informa Healthcare and published by CRC Press. This book was released on 2006-03-15 with total page 3656 pages. Available in PDF, EPUB and Kindle. Book excerpt: The previous edition of the International Encyclopedia of Ergonomics and Human Factors made history as the first unified source of reliable information drawn from many realms of science and technology and created specifically with ergonomics professionals in mind. It was also a winner of the Best Reference Award 2002 from the Engineering Libraries

Book Guidance and Control Design for High Speed Rollout and Turnoff  ROTO

Download or read book Guidance and Control Design for High Speed Rollout and Turnoff ROTO written by and published by . This book was released on 1996 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Predictive Features of a Cockpit Traffic Display

Download or read book Predictive Features of a Cockpit Traffic Display written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-10-18 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Eighteen pilots flew a series of traffic avoidance maneuvers in an experiment designed to assess the support offered and workload imposed by different levels of traffic display information in a free flight simulation. Three display prototypes were compared which differed in traffic information provided. A BASELINE (BL) display provided current and (2nd order) predicted information regarding ownship and current information of an intruder aircraft, represented on lateral and vertical displays in a coplanar suite. An INTRUDER PREDICTOR (IP) display, augmented the baseline display by providing lateral and vertical prediction of the intruder aircraft. A THREAT VECTOR (TV) display added to the IP display a vector that indicates the direction from ownship to the intruder at the predicted point of closest contact (POCC). The length of the vector corresponds to the radius of the protected zone, and the distance of the intersection of the vector with ownship predictor, corresponds to the time available till POCC or loss of separation. Pilots time shared the traffic avoidance task with a secondary task requiring them to monitor the top of the display for faint targets. This task simulated the visual demands of out-of-cockpit scanning, and hence was used to estimate the head-down time required by the different display formats. The results revealed that both display augmentations improved performance (safety) as assessed by predicted and actual loss of separation (i.e., penetration of the protected zone). Both enhancements also reduced workload, as assessed by the NASA TLX scale. The intruder predictor display produced these benefits with no substantial impact on the qualitative nature of the avoidance maneuvers that were selected. The threat vector produced the safety benefits by inducing a greater degree of (effective) lateral maneuvering, thus partially offsetting the benefits of reduced workload. The three displays did not differ in terms of their effect on performance of th...

Book Runway Incursion Prevention System Ads B and Dgps Data Link Analysis Dallas Fort Worth International Airport

Download or read book Runway Incursion Prevention System Ads B and Dgps Data Link Analysis Dallas Fort Worth International Airport written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-04 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A Runway Incursion Prevention System (RIPS) was tested at the Dallas - Ft. Worth International Airport in October 2000. The system integrated airborne and ground components to provide both pilots and controllers with enhanced situational awareness, supplemental guidance cues, a real-time display of traffic information, and warning of runway incursions in order to prevent runway incidents while also improving operational capability. Rockwell Collins provided and supported a prototype Automatic Dependent Surveillance - Broadcast (ADS-B) system using 1090 MHz and a prototype Differential GPS (DGPS) system onboard the NASA Boeing 757 research aircraft. This report describes the Rockwell Collins contributions to the RIPS flight test, summarizes the development process, and analyzes both ADS-B and DGPS data collected during the flight test. In addition, results are report on interoperability tests conducted between the NASA Advanced General Aviation Transport Experiments (AGATE) ADS-B flight test system and the NASA Boeing 757 ADS-B system.Timmerman, J. and Jones, Denise R. (Technical Monitor)Langley Research CenterDATA LINKS; FLIGHT TESTS; RUNWAYS; SURVEILLANCE; ACCIDENT PREVENTION; COLLISION AVOIDANCE; REAL TIME OPERATION; SITUATIONAL AWARENESS; DATA ACQUISITION; INSTALLING

Book Automated Landing  Rollout  and Turnoff Using MLS and Magnetic Cable Sensors

Download or read book Automated Landing Rollout and Turnoff Using MLS and Magnetic Cable Sensors written by S. Pines and published by . This book was released on 1977 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: A description of the simulation program used to study the landing approach, rollout and turnoff of the B737-100 aircraft utilizing MLS and a buried magnetic leader cable as navigation aids is presented. Simulation results are given and show the concept to be both feasible and practical for commercial type aircraft terminal area control.