2020
DOI: 10.2514/1.c035458
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Aircraft Performance Model Calibration and Validation for General Aviation Safety Analysis

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Cited by 6 publications
(1 citation statement)
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“…Proximity to buildings [35], flying over people [15], navigating unmapped areas algorithm properties. Fixed-wing aircraft typically optimize cruise altitude (atmospheric density), airspeed, climb rate, lift/drag ratio [36,37], and hazardous weather avoidance [38] but do not consider ground-based obstacles due to their substantial cruise altitude. Multicopter UAS operate at much lower altitudes thus typically optimize motions over clearance from obstacles, distance / time, and mission requirements [39].…”
Section: Environmentmentioning
confidence: 99%
“…Proximity to buildings [35], flying over people [15], navigating unmapped areas algorithm properties. Fixed-wing aircraft typically optimize cruise altitude (atmospheric density), airspeed, climb rate, lift/drag ratio [36,37], and hazardous weather avoidance [38] but do not consider ground-based obstacles due to their substantial cruise altitude. Multicopter UAS operate at much lower altitudes thus typically optimize motions over clearance from obstacles, distance / time, and mission requirements [39].…”
Section: Environmentmentioning
confidence: 99%