2010
DOI: 10.2514/1.47146
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Wingbeat Shape Modulation for Flapping-Wing Micro-Air-Vehicle Control During Hover

Abstract: The public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for … Show more

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Cited by 168 publications
(101 citation statements)
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“…However, many simulations such as the one shown in figure 4 indicate that the system (8) is stable. Figure 4 shows that direct application of the averaging theorem is not sufficient to analyze the stability of the system (8). It should be noted that the timeinvariant systems obtained through direct averaging of (8) and the original hovering flight dynamics (4) are the same.…”
Section: Direct Averaging Approachmentioning
confidence: 99%
See 4 more Smart Citations
“…However, many simulations such as the one shown in figure 4 indicate that the system (8) is stable. Figure 4 shows that direct application of the averaging theorem is not sufficient to analyze the stability of the system (8). It should be noted that the timeinvariant systems obtained through direct averaging of (8) and the original hovering flight dynamics (4) are the same.…”
Section: Direct Averaging Approachmentioning
confidence: 99%
“…In this subsection, we show that second-order averaging is able to more accurately capture the stability characteristics of the example considered in the last section (hovering dynamics with fixed point), which is presented in equation (8).…”
Section: Hovering Dynamics Omitting the Periodic External Forcing: Fimentioning
confidence: 99%
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