Rapid area change in pitch-up manoeuvres of small perching birds

• Published in: Bioinspiration & biomimetics Vol. 10; no. 6; p. 066004
• Main Authors: Polet, D T, Rival, D E
• Format: Journal Article
• Language: English
• Published: England IOP Publishing 26.10.2015
• Subjects: Acceleration; aerodynamics; Aircraft - instrumentation; Animals; Biological Clocks - physiology; Biomimetics; Biomimetics - instrumentation; Biomimetics - methods; bird flight; Birds - physiology; Computer Simulation; Deceleration; Dissipation; Drag; Energy Transfer - physiology; Flight, Animal - physiology; Landing; Lift; Mathematical analysis; micro aerial vehicles; Models, Biological; perching; Posture - physiology; Potential energy; rapid area change; Robotics - instrumentation; Shear Strength - physiology; Wings, Animal - physiology
• ISSN: 1748-3190; 1748-3182; 1748-3190
• DOI: 10.1088/1748-3190/10/6/066004

Rapid pitch-up has been highlighted as a mechanism to generate large lift and drag during landing manoeuvres. However, pitching rates had not been measured previously in perching birds, and so the direct applicability of computations and experiments to observed behaviour was not known. We measure pitch rates in a small, wild bird (the black-capped chickadee; Poecile atricapillus), and show that these rates are within the parameter range used in experiments. Pitching rates were characterized by the shape change number, a metric comparing the rate of frontal area increase to acceleration. Black-capped chickadees increase the shape change number during perching in direct proportion to their total kinetic and potential energy at the start of the manoeuvre. The linear relationship between dissipated energy and shape change number is in accordance with a simple analytical model developed for two-dimensional pitching and decelerating airfoils. Black-capped chickadees use a wing pitch-up manoeuvre during perching to dissipate energy quickly while maintaining lift and drag through rapid area change. It is suggested that similar pitch-and-decelerate manoeuvres could be used to aid in the controlled, precise landings of small manoeuvrable air vehicles.