17th AIAA Aviation Technology, Integration, and Operations Conference 2017
DOI: 10.2514/6.2017-4095
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Flight Crew Survey Responses from the Interval Management (IM) Avionics Phase 2 Flight Test

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Cited by 9 publications
(12 citation statements)
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“…Although the spacing performance was satisfactory, operational issues that are barely identifiable outside an HITL environment were found in terms of the number, frequency, and timing of speed commands, their magnitude (step size), and overall energy management. [7][8][9] The parameters measured in our simulation (described in Section 3.11) were selected to quantify these findings.…”
Section: Flight Test Resultsmentioning
confidence: 99%
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“…Although the spacing performance was satisfactory, operational issues that are barely identifiable outside an HITL environment were found in terms of the number, frequency, and timing of speed commands, their magnitude (step size), and overall energy management. [7][8][9] The parameters measured in our simulation (described in Section 3.11) were selected to quantify these findings.…”
Section: Flight Test Resultsmentioning
confidence: 99%
“…Furthermore, a qualitative flight crew survey conducted during a flight test in February 2017 indicated that the system has not yet attained an operationally implementable level owing to issues related to workload and acceptance. [7][8][9] This was reflected by negative feedback comments such as "Too many speed changes," "Large decelerations" (speed steps well over 40 kt), and "inefficient IM speed reversals" (speed commands negating the effect of a previous command). Previous studies have primarily focused on the goal time observation or the string stability of multiple aircraft engaged in FIM, 10) while usability factors have rarely been considered.…”
Section: Introductionmentioning
confidence: 99%
“…In this study, two scoring attributes and three penalty attributes, influenced by the results of Refs. (23)(24)(25), were employed. The final score (S) is determined from the sum of all individual scores (s k ) multiplied by an optional corresponding weight factor (q k ).…”
Section: Cost Functionmentioning
confidence: 99%
“…NASA's research on ASTAR was concluded in early 2017 with a final flight test (23)(24)(25) . While sophisticated spacing capability of FIM could be confirmed, pilots' comments highlighted the operational difficulties such as 'too many IM speed changes, or the rate of the speed changes is too high' (24) , and the crew had 'no fore-knowledge of when or what the next IM speed would be' and 'could only be reactive'.…”
Section: Introductionmentioning
confidence: 99%
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