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Analysis of the Impact of Orbit-Attitude Coupling at Higher-Degree Potential Models on Spacecraft Dynamics

The Journal of the astronautical sciences, 2022, Vol.69 (4), p.955-987

2022

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Unscented Kalman filter and control on TSE(3) with application to spacecraft dynamics

Nonlinear dynamics, 2022-05, Vol.108 (3), p.2127-2146

2022

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Fuel efficient periodic gain control strategies for spacecraft relative motion in elliptic chief orbits

International journal of dynamics and control, 2016-03, Vol.4 (1), p.104-122

2016

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Rigid-Body Noncertainty Equivalence Adaptive Control on the Tangent Bundle of SE(3)

Journal of guidance, control, and dynamics, 2023-10, Vol.46 (10), p.1892-1900

2023

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Disturbance observer-based nonlinear feedback control for position tracking of electro-hydraulic systems in a finite time

European journal of control, 2022-09, Vol.67, p.100659, Article 100659

2022

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Numerical Approaches for Constrained and Unconstrained, Static Optimization on the Special Euclidean Group SE(3)

Journal of optimization theory and applications, 2024-06, Vol.201 (3), p.1116-1150

2024

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Control and maintenance of fully-constrained and underconstrained rigid body motion on Lie groups and their tangent bundles

Journal of geometric mechanics, 2022-03, Vol.14 (1), p.29

2022

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Coefficient of restitution in fractional viscoelastic compliant impacts using fractional Chebyshev collocation

Journal of sound and vibration, 2017-02, Vol.388, p.230-244

2017

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Optimal Periodic-Gain Fractional Delayed State Feedback Control for Linear Fractional Periodic Time-Delayed Systems

IEEE transactions on automatic control, 2018-04, Vol.63 (4), p.989-1002

2018

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Utilizing the geometric mechanics framework to predict attitude in a full ephemeris model of the Cislunar region

Communications in nonlinear science & numerical simulation, 2024-03, Vol.130, p.107726, Article 107726

2024

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Decentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay

Journal of guidance, control, and dynamics, 2016-04, Vol.39 (4), p.838-851

2016

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Circular restricted full three-body problem with rigid-body spacecraft dynamics in binary asteroid systems

Celestial mechanics and dynamical astronomy, 2024-04, Vol.136 (2), p.9, Article 9

2024

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Framework for the full N-body problem in SE(3) and its reduction to the circular restricted full three-body problem

Celestial mechanics and dynamical astronomy, 2023-08, Vol.135 (4), p.41, Article 41

2023

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Unscented Kalman filter and control on $$\mathsf {TSE(3)}$$ with application to spacecraft dynamics

Nonlinear dynamics, 2022-05, Vol.108 (3), p.2127-2146

2022

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Mass property estimation on TSE(3) via unscented Kalman filter using RCS thrusters

Acta astronautica, 2024-10, Vol.223, p.462-480

2024

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Fuel Efficiency of Fully and Underconstrained Coulomb Formations in Slightly Elliptic Reference Orbits

IEEE transactions on aerospace and electronic systems, 2021-12, Vol.57 (6), p.4171-4187

2021

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Spacecraft Attitude Fractional Feedback Control Using Rotation Matrices and Exponential Coordinates

Journal of guidance, control, and dynamics, 2018-10, Vol.41 (10), p.2185-2198

2018

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Spacecraft Attitude Stabilization Using Nonlinear Delayed Multiactuator Control and Inverse Dynamics

Journal of guidance, control, and dynamics, 2013-09, Vol.36 (5), p.1440-1452

2013

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Transition Curve Analysis of Linear Fractional Periodic Time-Delayed Systems Via Explicit Harmonic Balance Method

Journal of computational and nonlinear dynamics, 2016-07, Vol.11 (4)

2016

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Nonlinear vibration analysis of isotropic cantilever plate with viscoelastic laminate

Nonlinear dynamics, 2009-06, Vol.56 (4), p.325-356

2009

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On the stability and bifurcation analysis of dual-spin spacecraft

Acta astronautica, 2014-01, Vol.93, p.162-175

2014

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Fractional delayed damped Mathieu equation

International journal of control, 2015-03, Vol.88 (3), p.622-630

2015

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Analysis of stability and Hopf bifurcation of delayed feedback spin stabilization of a rigid spacecraft

Nonlinear dynamics, 2013-11, Vol.74 (3), p.801-817

2013

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Fuel efficient periodic gain control strategies for spacecraft relative motion in elliptic chief orbits

International journal of dynamics and control, 2016, Vol.4 (1), p.104-122

2016

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Earth–Moon L1 libration point orbit continuous stationkeeping control using time-varying LQR and backstepping

International journal of dynamics and control, 2017-12, Vol.5 (4), p.1089-1102

2017

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Analysis of the Impact of Orbit-Attitude Coupling at Higher-Degree Potential Models on Spacecraft Dynamics

Unscented Kalman filter and control on TSE(3) with application to spacecraft dynamics

Fuel efficient periodic gain control strategies for spacecraft relative motion in elliptic chief orbits

Rigid-Body Noncertainty Equivalence Adaptive Control on the Tangent Bundle of SE(3)

Disturbance observer-based nonlinear feedback control for position tracking of electro-hydraulic systems in a finite time

Numerical Approaches for Constrained and Unconstrained, Static Optimization on the Special Euclidean Group SE(3)

Control and maintenance of fully-constrained and underconstrained rigid body motion on Lie groups and their tangent bundles

Coefficient of restitution in fractional viscoelastic compliant impacts using fractional Chebyshev collocation

Optimal Periodic-Gain Fractional Delayed State Feedback Control for Linear Fractional Periodic Time-Delayed Systems

Utilizing the geometric mechanics framework to predict attitude in a full ephemeris model of the Cislunar region

Decentralized Consensus Control of a Rigid-Body Spacecraft Formation with Communication Delay

Circular restricted full three-body problem with rigid-body spacecraft dynamics in binary asteroid systems

Framework for the full N-body problem in SE(3) and its reduction to the circular restricted full three-body problem

Unscented Kalman filter and control on $$\mathsf {TSE(3)}$$ with application to spacecraft dynamics

Mass property estimation on TSE(3) via unscented Kalman filter using RCS thrusters

Fuel Efficiency of Fully and Underconstrained Coulomb Formations in Slightly Elliptic Reference Orbits

Spacecraft Attitude Fractional Feedback Control Using Rotation Matrices and Exponential Coordinates

Spacecraft Attitude Stabilization Using Nonlinear Delayed Multiactuator Control and Inverse Dynamics

Transition Curve Analysis of Linear Fractional Periodic Time-Delayed Systems Via Explicit Harmonic Balance Method

Nonlinear vibration analysis of isotropic cantilever plate with viscoelastic laminate

On the stability and bifurcation analysis of dual-spin spacecraft

Fractional delayed damped Mathieu equation

Analysis of stability and Hopf bifurcation of delayed feedback spin stabilization of a rigid spacecraft

Fuel efficient periodic gain control strategies for spacecraft relative motion in elliptic chief orbits

Earth–Moon L1 libration point orbit continuous stationkeeping control using time-varying LQR and backstepping

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