2015
DOI: 10.2514/1.c032682
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Fixed-Wing Unmanned Aircraft In-Flight Pitch and Yaw Control Moment Sensing

Abstract: Unsteady, nonlinear aerodynamics at high angles of attack challenges small unmanned aircraft system autopilots that rely heavily on inertial-based instrumentation. This work introduces an expanded aerodynamic sensing system for poststall flight conditions that incorporate high angle of attack and prop-wash aerodynamic forces based on in-flight measurement. A flight vehicle with a 1.8 m wingspan is used in wind-tunnel tests to measure the pitch and yaw moments due to freestream and prop-wash over the tail surfa… Show more

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Cited by 10 publications
(5 citation statements)
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“…Learning to minimize stall distance on the fly requires aeromechanical information (for example, from feather 1 , 2 or muscle 39 proprioceptors) and distance information (for example, from static visual 5 or optic flow 7 , 11 , 40 cues) to be combined. Fly-by-feel concepts 41 – 45 may therefore prove critical to the learning and control of perching in autonomous vehicles. Moreover, it seems likely that our birds would have learned the optimized position of the transition point as a virtual target for trajectory control, analogous to the ‘entry gate’ approach adopted in one recent implementation of autonomous perching 18 .…”
Section: Discussionmentioning
confidence: 99%
“…Learning to minimize stall distance on the fly requires aeromechanical information (for example, from feather 1 , 2 or muscle 39 proprioceptors) and distance information (for example, from static visual 5 or optic flow 7 , 11 , 40 cues) to be combined. Fly-by-feel concepts 41 – 45 may therefore prove critical to the learning and control of perching in autonomous vehicles. Moreover, it seems likely that our birds would have learned the optimized position of the transition point as a virtual target for trajectory control, analogous to the ‘entry gate’ approach adopted in one recent implementation of autonomous perching 18 .…”
Section: Discussionmentioning
confidence: 99%
“…Because the aerodynamic forces that perturb flight can be sensed before any measurable disturbance to the kinematic state of the system has had time to evolve, force feedback has a lower latency than state feedback 40,41 . This is a key attraction of fly-by-feel concepts in experimental autonomous vehicles 42 , which have demonstrated some notable successes in gust rejection 43,44 . Our modelling hints at an unexpected role for force feedback in perching, analogous to the role of accelerometer feedback in coordinating turns in high-performance aircraft 45 .…”
Section: Minimizing Either Time or Energy Requires Very High Lift Coefficientsmentioning
confidence: 98%
“…Controlling these optimized parameter settings in open loop would be susceptible to external disturbances and internal error, but muscle power output is expected to be regulated locally under strain rate feedback from the muscle spindle cells 39 , and the lift force communicated to the body 41 may be regulated locally under force feedback from the muscle Golgi tendon organs 39 . Analogous “fly-by-feel” concepts 42 have demonstrated some notable successes in gust rejection in small air vehicles 43,44 , and may therefore prove important to controlling perching given the low-latency feedback that they provide 45,46 . Furthermore, given the physical significance of the transition point, which was always located at approximately 60% of perch spacing distance, it seems plausible that this learned optimum could have served as a virtual target for closed-loop trajectory control under visual feedback.…”
mentioning
confidence: 99%
“…Some modern flying vehicles already use arrays of lowbandwidth anemometers for flow sensing [16,82,83]. These sensor arrays can be, for example, shear stress sensors embedded in a flexible skin [84], pressure ports distributed over the body or wings [56,[84][85][86], or hot-film sensors distributed over the wing [87]. Some sensors have narrow frequency responses, like the microelectromechanical system (MEMS) sensor array modelled after cricket hairs (peak response at 75 Hz [88]).…”
Section: Convergence Is Accelerated By Multiple Lowbandwidth Anemometersmentioning
confidence: 99%