activity
20152026
most citedDiscrete-time optimal attitude control of spacecraft with momentum and control constraints

21 citations · 52 across the 33 of their papers we have counts for

collaborators
Showing 2017Show all

9 papers · 1 filter

eess.SY2017

Structure-preserving discrete-time optimal maneuvers of a wheeled inverted pendulum

Karmvir Singh Phogat, Ravi Banavar, Debasish Chatterjee

The Wheeled Inverted Pendulum (WIP) is a nonholonomic, underactuated mechanical system, and has been popularized commercially as the {\it Segway}. Designing optimal control laws fo…

eess.SY2017

Almost-global tracking of the unactuated joint in a pendubot

Aradhana Nayak, Ravi N. Banavar

Tracking the unactuated configuration variable in an underactuated system, in a global sense, has not received much attention. Here we present a scheme to do so for a pendubot - a…

eess.SY2017

Robust Attitude Tracking for Aerobatic Helicopters: A Geometric Approach

Nidhish Raj, Ravi N Banavar, Abhishek +1

This paper highlights the significance of the rotor dynamics in control design for small-scale aerobatic helicopters, and proposes two singularity free robust attitude tracking con…

eess.SY2017

Further insights into the damping-induced self-recovery phenomenon

Tejas Kotwal, Roshail Gerard, Ravi Banavar

In a series of papers, D. E. Chang, et al., proved and experimentally demonstrated a phenomenon they termed "damping-induced self-recovery". However, these papers left a few questi…

eess.SY2017

Control Synthesis for an Underactuated Cable Suspended System Using Dynamic Decoupling

Siddharth H. Nair, Ravi N. Banavar, D. H. S. Maithripala

This article studies the dynamics and control of a novel underactuated system, wherein a plate suspended by cables and with a freely moving mass on top, whose other ends are attach…

eess.SY2017

The Principal Fiber Bundle Structure of the Gimbal-Spacecraft System

Ravi N Banavar, Arjun Narayanan

The gimbal-spacecraft system, that consists of a variable speed control moment gyro (VSCMG) mounted inside a spacecraft, has been employed as an actuator for the attitude control o…

eess.SY2017

Attitude Tracking Control for Aerobatic Helicopters: A Geometric Approach

Nidhish Raj, Ravi N. Banavar, Abhishek +1

We consider the problem of attitude tracking for small-scale aerobatic helicopters. A small scale helicopter has two subsystems: the fuselage, modeled as a rigid body; and the roto…

eess.SY2017

Almost-global tracking for a rigid body with internal rotors

Aradhana Nayak, Ravi N. Banavar

Almost-global orientation trajectory tracking for a rigid body with external actuation has been well studied in the literature, and in the geometric setting as well. The tracking c…

eess.SY2017★ 4 cited

Trajectory Tracking Using Motion Primitives for the Purcell's Swimmer

Sudin Kadam, Kedar Joshi, Naman Gupta +2

Locomotion at low Reynolds numbers is a topic of growing interest, spurred by its various engineering and medical applications. This paper presents a novel prototype and a locomoti…