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Stabilization of Energy-Conserving Gaits for Point-Foot Planar Bipeds

Aakash Khandelwal, Nilay Kant, Ranjan Mukherjee

Abstract

The problem of designing and stabilizing impact-free, energy-conserving gaits is considered for underactuated, point-foot planar bipeds. Virtual holonomic constraints are used to design energy-conserving gaits. A desired gait corresponds to a periodic hybrid orbit and is stabilized using the Impulse Controlled Poincaré Map approach. Numerical simulations for the case of a five-link biped demonstrate convergence to a desired gait from arbitrary initial conditions.

Stabilization of Energy-Conserving Gaits for Point-Foot Planar Bipeds

Abstract

The problem of designing and stabilizing impact-free, energy-conserving gaits is considered for underactuated, point-foot planar bipeds. Virtual holonomic constraints are used to design energy-conserving gaits. A desired gait corresponds to a periodic hybrid orbit and is stabilized using the Impulse Controlled Poincaré Map approach. Numerical simulations for the case of a five-link biped demonstrate convergence to a desired gait from arbitrary initial conditions.
Paper Structure (20 sections, 47 equations, 6 figures, 2 tables)

This paper contains 20 sections, 47 equations, 6 figures, 2 tables.

Figures (6)

  • Figure 1: An $n$-link point-foot planar biped.
  • Figure 2: Hybrid dynamics of biped over a step with a single impulsive actuation during the swing phase. The different components are: $1 $: continuous-time dynamics, $2 $: jump in states due to impulsive actuation, $3 $: jump in states due to foot-ground in interaction, and $4 $: change of states due to coordinate relabelling.
  • Figure 3: Hybrid dynamics of biped over a step for an energy-conserving gait; it is a simpler version of the dynamics shown in Fig.\ref{['Fig2']}. The different components are: $1 $: continuous-time dynamics, $4 $: change of states due to coordinate relabelling.
  • Figure 4: Evolution of system trajectory during an energy-conserving gait.
  • Figure 5: Schematic of the ICPM approach to orbital stabilization of an energy-conserving gait. The desired orbit is shown in red. The different components of the hybrid dynamics, namely, $1 $, $2 $, $3 $ and $4 $ are described by \ref{['eq13']}.
  • ...and 1 more figures

Theorems & Definitions (4)

  • Remark 1
  • Remark 2
  • Remark 3
  • Remark 4