activity
20212025
most citedNonlinear Control Allocation Using A Piecewise Multi-Linear Representation

6 citations · 10 across the 7 of their papers we have counts for

collaborators
Showing eess.SYShow all

8 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★ 6 cited

Nonlinear Control Allocation Using A Piecewise Multi-Linear Representation

Jahanzeb Rajput, Hafiz Zeeshan Iqbal Khan

Nonlinear control allocation is an important part of modern nonlinear dynamic inversion based flight control systems which require highly accurate model of aircraft aerodynamics. G…

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…