By Jared A Grauer
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Additional resources for Flight dynamics and system identification for modern feedback control: Avian-inspired robots
Chapter 5 presents ﬂight simulation results obtained using the ﬂight dynamics model developed in Chapters 3 and 4. A method for determining trim solutions is presented and is employed to trim the ornithopter model for straight and level mean ﬂight. The model is then linearized about the trim trajectory, resulting in a canonical time-invariant model as well as a time-periodic model. Feedback control laws are then designed for the ornithopter longitudinal dynamics that could be implemented in an autopilot.
Liu, Aerodynamics of Low Reynolds Number Flyers, Cambridge Aerospace Series. Cambridge University Press, 2007. D. Keats-Pullen, J. Hubbard, and N. Guerreiro, “Spatial weighting of smart materials for real-time measurement of aerodynamic forces”, Journal of Intelligent Material Systems and Structures, vol. 19, no. 7, pp. 837–844, July 2007. M. Bolender, “Rigid multi-body equations-of-motion for ﬂapping wing mavs using kane’s equations”, Chicago, IL, August 2009, AIAA, Guidance, Navigation, and Control Conference.
Benedict, and I. Chopra, “Experimental investigation of a ﬂapping wing concept in hoverand forward ﬂight for micro air vehicle applications”, Phoenix, AZ, May 2010, American Helicopter Society, 66th Annual Forum. 8. P. Seshadri, M. Benedict, and I. Chopra, “Experimental investigation of an insect-based ﬂapping wing hovering 129 Flight dynamics and system identiﬁcation 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. micro air vehicle”, San Francisco, CA, January 2010, American Helicopter Society, Aeromechanics Specialists’ Conference.