AIAA Guidance, Navigation, and Control Conference and Exhibit 2005
DOI: 10.2514/6.2005-6139
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Investigation of a Three-Degree Decelerating Approach of a Twin-Engined Jet Aircraft under Actual Flight Conditions

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Cited by 5 publications
(3 citation statements)
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“…A first solution could be to have a constant time scale and create minimum/maximum ETA cues able to move, as the ETA cue. Moreover, it was recommended that the flap/gear cues should be more discernible, and maybe they can be presented on the PFD [23]. In addition, the cues on the trajectory line, regarding the early/delayed deceleration, should be reconsidered, so a cue leading to the optimum solution may be presented too or to provide a shorter solution space for all the IAS commands, not just for the next one.…”
Section: Discussionmentioning
confidence: 99%
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“…A first solution could be to have a constant time scale and create minimum/maximum ETA cues able to move, as the ETA cue. Moreover, it was recommended that the flap/gear cues should be more discernible, and maybe they can be presented on the PFD [23]. In addition, the cues on the trajectory line, regarding the early/delayed deceleration, should be reconsidered, so a cue leading to the optimum solution may be presented too or to provide a shorter solution space for all the IAS commands, not just for the next one.…”
Section: Discussionmentioning
confidence: 99%
“…This concept was tested in computer simulations using aircraft performance data [14], [15], [18], [30] in European airports varying in traffic load. In addition, more realistic conditions were examined in actual flight tests [4], [6], [10], [23] and sessions in flight simulators [6], [12], [13]. The procedure of CDA has been adapted to different forms, by modifying its parameters.…”
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confidence: 99%
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