A dynamics and stability framework for avian jumping take-off. Issue 10 (31st October 2018)

• Record Type: Journal Article
• Authors: Parslew, Ben; Sivalingam, Girupakaran; Crowther, William
• Is Part Of: Royal Society open science. Volume 5:Issue 10(2018)
• Publication Date: 2018-10-31
• Subjects: jumping -- flight stability -- take-off -- animal flight -- aerodynamics -- jumping robots; Science -- Periodicals; 500
• DOI: 10.1098/rsos.181544
• Languages: English
• ISSNs: 2054-5703

Abstract

Abstract : Jumping take-off in birds is an explosive behaviour with the goal of providing a rapid transition from ground to airborne locomotion. An effective jump is predicated on the need to maintain dynamic stability through the acceleration phase. The present study concerns understanding how birds retain control of body attitude and trajectory during take-off. Cursory observation suggests that stability is achieved with relatively little cost. However, analysis of the problem shows that the stability margins during jumping are actually very small and that stability considerations play a significant role in the selection of appropriate jumping kinematics. We use theoretical models to understand stability in prehensile take-off (from a perch) and also in non-prehensile take-off (from the ground). The primary instability is tipping, defined as rotation of the centre of gravity about the ground contact point. Tipping occurs when the centre of pressure falls outside the functional foot. A contribution of the paper is the development of graphical tipping stability margins for both centre of gravity location and acceleration angle. We show that the nose-up angular acceleration extends stability bounds forward and is hence helpful in achieving shallow take-offs. The stability margins are used to interrogate simulated take-offs of real birds using published experimental kinematic data from a guinea fowl (ground take-off) and a diamond dove (perch take-off). For the guinea fowl, the initial part of the jump is stable; however, simulations exhibit a stuttering instability not observed experimentally that is probably due to the absence of compliance in the idealized joints. The diamond dove model confirms that the foot provides an active torque reaction during take-off, extending the range of stable jump angles by around 45°.