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

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Showing 2015Show all

5 papers · 1 filter

math.DS2015

Circular orbit spacecraft control at the L4 point using Lyapunov functions

Rachana Agrawal, Ravi N Banavar

The objective of this work is to demonstrate the utility of Lyapunov functions in control synthesis for the purpose of maintaining and stabilizing a spacecraft in a circular orbit…

eess.SY2015★ 2 cited

A geometric approach to the dynamics of flapping wing micro aerial vehicles: Modelling and reduction

Sudin Kadam, Sneha Gajbhiye, Ravi Banavar

This paper presents a geometric framework for analysis of dynamics of flapping wing micro aerial vehicles (FWMAV) which achieve locomotion in the special Euclidean group SE(3) usin…

eess.SY2015★ 1 cited

Almost-globally stable tracking for on compact Riemannian manifolds

Aradhana Nayak, Ravi Banavar

In this article, we propose a control law for almost-global asymptotic tracking (AGAT) of a smooth reference trajectory for a fully actuated simple mechanical system (SMS) evolving…

eess.SY2015★ 4 cited

Geometric approach to tracking and stabilization for a spherical robot actuated by internal rotors

Sneha Gajbhiye, Ravi N. Banavar

This paper presents tracking control laws for two different objectives of a nonholonomic system - a spherical robot - using a geometric approach. The first control law addresses or…

eess.SY2015★ 21 cited

Discrete-time optimal attitude control of spacecraft with momentum and control constraints

Karmvir Singh Phogat, Debasish Chatterjee, Ravi Banavar

This article solves an optimal control problem arising in attitude control of a spacecraft under state and control constraints. We first derive the discrete-time attitude dynamics…