activity
20152024
most citedDiscrete-time optimal attitude control of spacecraft with momentum and control constraints

21 citations · 40 across the 9 of their papers we have counts for

collaborators

12 papers

cs.CL2024

Fine-tuning Smaller Language Models for Question Answering over Financial Documents

Karmvir Singh Phogat, Sai Akhil Puranam, Sridhar Dasaratha +2

Recent research has shown that smaller language models can acquire substantial reasoning abilities when fine-tuned with reasoning exemplars crafted by a significantly larger teache…

cs.CL2023★ 3 cited

Zero-Shot Question Answering over Financial Documents using Large Language Models

Karmvir Singh Phogat, Chetan Harsha, Sridhar Dasaratha +2

We introduce a large language model (LLM) based approach to answer complex questions requiring multi-hop numerical reasoning over financial reports. While LLMs have exhibited remar…

eess.SY2021

DeepPSL: End-to-end perception and reasoning

Sridhar Dasaratha, Sai Akhil Puranam, Karmvir Singh Phogat +2

We introduce DeepPSL a variant of probabilistic soft logic (PSL) to produce an end-to-end trainable system that integrates reasoning and perception. PSL represents first-order logi…

math.OC2020★ 1 cited

Tracking Controller Design for Satellite Attitude Under Unknown Constant Disturbance Using Stable Embedding

Wonshick Ko, Karmvir Singh Phogat, Nicolas Petit +1

We propose a tracking control law for the fully actuated rigid body system in the presence of any unknown constant disturbance by employing quaternions with the stable embedding te…

math.OC2019

Invariant extended Kalman filter on matrix Lie groups

Karmvir Singh Phogat, Dong Eui Chang

We derive symmetry preserving invariant extended Kalman filters (IEKF) on matrix Lie groups. These Kalman filters have an advantage over conventional extended Kalman filters as the…

math.OC2019★ 14 cited

Model Predictive Tracking Control for Invariant Systems on Matrix Lie Groups via Stable Embedding into Euclidean Spaces

Dong Eui Chang, Karmvir Singh Phogat, Jongeun Choi

For controller design for systems on manifolds embedded in Euclidean space, it is convenient to utilize a theory that requires a single global coordinate system on the ambient Eucl…

eess.SY2019

Exact isoholonomic motion of the planar Purcell's swimmer

Sudin Kadam, Karmvir Singh Phogat, Ravi N. Banavar +1

In this article we present the discrete-time isoholonomic problem of the planar Purcell's swimmer and solve it using the Discrete-time Pontryagin maximum principle. The 3-link Purc…

eess.SY2018★ 1 cited

Structure-Preserving Constrained Optimal Trajectory Planning of a Wheeled Inverted Pendulum

Klaus Albert, Karmvir Singh Phogat, Felix Anhalt +3

The Wheeled Inverted Pendulum (WIP) is an underactuated, nonholonomic mechatronic system, and has been popularized commercially as the Segway. Designing a control law for motion pl…

eess.SY2018

A frequency-constrained geometric Pontryagin maximum principle on matrix Lie groups

Shruti Kotpalliwar, Pradyumna Paruchuri, Karmvir Singh Phogat +2

In this article we present a geometric discrete-time Pontryagin maximum principle (PMP) on matrix Lie groups that incorporates frequency constraints on the controls in addition to…

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.SY2016

A discrete-time Pontryagin maximum principle on matrix Lie groups

Karmvir Singh Phogat, Debasish Chatterjee, Ravi Banavar

In this article we derive a Pontryagin maximum principle (PMP) for discrete-time optimal control problems on matrix Lie groups. The PMP provides first order necessary conditions fo…

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…