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20212025
most citedAirfoil's Aerodynamic Coefficients Prediction using Artificial Neural Network

37 citations · 43 across the 8 of their papers we have counts for

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7 papers · 1 filter

eess.SY2025

Geometrization of Higher-Order Linear Control Laws for Attitude Control on

Farooq Aslam, Hafiz Zeeshan Iqbal Khan, Muhammad Farooq Haydar +2

This paper presents a theoretical framework for analyzing the stability of higher-order geometric nonlinear control laws for attitude control on the Special Orthogonal Group $\math…

eess.SY2024

Rigid-Body Attitude Control on using Nonlinear Dynamic Inversion

Hafiz Zeeshan Iqbal Khan, Farooq Aslam, Muhammad Farooq Haydar +1

This paper presents a cascaded control architecture, based on nonlinear dynamic inversion (NDI), for rigid body attitude control. The proposed controller works directly with the ro…

eess.SY2023

Robust Stability Analysis of a Class of LTV Systems

Shahzad Ahmed, Hafiz Zeeshan Iqbal Khan, Jamshed Riaz

Many physical systems are inherently time-varying in nature. When these systems are linearized around a trajectory, generally, the resulting system is Linear Time-Varying (LTV). LT…

eess.SY2023

Modelling, Simulation, and Control of a Flexible Space Launch Vehicle

Muhammad Abdullah Aamer, Qurat Ul Ain, Ushbah Kaleem +2

Modern Space Launch Vehicles (SLVs), being slender in shape and due to the use of lightweight materials, are generally flexible in nature. This structural flexibility, when coupled…

eess.SY2022★ 4 cited

Reconfigurable Control of a Class of Multicopters

Hafiz Zeeshan Iqbal Khan, Jahanzeb Rajput, Jamshed Riaz

In this paper, a reconfigurable control scheme for a generalized class of multicopters is presented to overcome single or multiple rotor failures. In a multicopter, the rotor failu…

eess.SY2022★ 2 cited

Nonlinear Control Allocation: A Learning Based Approach

Hafiz Zeeshan Iqbal Khan, Surrayya Mobeen, Jahanzeb Rajput +1

Modern aircraft are designed with redundant control effectors to cater for fault tolerance and maneuverability requirements. This leads to aircraft being over-actuated and requires…

eess.SY2021

Robust Stability Analysis of an Uncertain Aircraft Model with Scalar Parametric Uncertainty

Farooq Aslam, Fatima Shoaib, Hafiz Zeeshan Iqbal Khan +2

A robust controller is specified, and the stability bounds of the uncertain closed-loop system are determined using the small gain, circle, positive real, and Popov criteria. A gra…