2017
DOI: 10.2514/1.g001756
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Intelligent Flight Control Systems Evaluation for Loss-of-Control Recovery and Prevention

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Cited by 16 publications
(8 citation statements)
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“…Joint points of the head and foot are extracted by horizontal line scanning algorithm, joint points of the knee, hip, neck, and chest are extracted by length proportion constraint, and joint points of the hand, elbow, and shoulder are extracted by vertical scanning algorithm [18,19] e internal structure of physical training includes body shape, body function, sports quality, and health level [20].…”
Section: Human Pose Estimation Based On Contour Edgementioning
confidence: 99%
“…Joint points of the head and foot are extracted by horizontal line scanning algorithm, joint points of the knee, hip, neck, and chest are extracted by length proportion constraint, and joint points of the hand, elbow, and shoulder are extracted by vertical scanning algorithm [18,19] e internal structure of physical training includes body shape, body function, sports quality, and health level [20].…”
Section: Human Pose Estimation Based On Contour Edgementioning
confidence: 99%
“…Upset Prevention and Recovery Training (UPRT) is one example of such scenario [14], where adequate simulation training can help reduce loss of control in-flight (LOC-I), a significant contributor to fatal accidents [15,16]. Various efforts have been undertaken to reduce LOC-I, such as predictive cueing [17], haptic feedback [18] and adaptive flight control systems [19,20]. In the European research project 'Simulation of Upset Recovery in Aviation' (SUPRA), centrifuge-based simulation has shown to significantly improve pilot's ability to recover from adverse flight attitudes [21][22][23].…”
Section: Introductionmentioning
confidence: 99%
“…In the research of the aircraft system, many papers on fault-tolerant and adaptive control methods are developed and demonstrated for LOC hazards mitigation [16], [17]. For example, reference [18] utilized a new intelligent flight control system to prevent the LOC and validated the effectiveness by conducting the pilotin-the-loop experiments. Reference [19] proposed a stable adaptive approach which is used in the simultaneous sensor, actuator, and slow-engine gain failure accommodation of the flight control.…”
Section: Introductionmentioning
confidence: 99%