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Adaptive Disturbance-Based High-Order Sliding-Mode Control for Hypersonic-Entry Vehicles

Journal of guidance, control, and dynamics, 2017-03, Vol.40 (3), p.521-536

2017

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Autonomous Trajectory Planning and Guidance Control for Launch Vehicles

1st Edition 2023, 2023

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Survey of autonomous guidance methods for powered planetary landing

Frontiers of information technology & electronic engineering, 2020-05, Vol.21 (5), p.652-674

2020

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Modeling of a Tethered Testbed for a VTVL Vehicle

Modelling and Simulation in Engineering, 2020-10, Vol.2020, p.1-13

2020

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Onboard Trajectory Generation for Entry Vehicles via Adaptive Multivariate Pseudospectral Interpolation

Journal of guidance, control, and dynamics, 2017-02, Vol.40 (2), p.466-476

2017

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Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex–Concave Decomposition

Journal of guidance, control, and dynamics, 2024-01, Vol.47 (1), p.20-35

2024

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Development of a low cost star tracker for the SHEFEX mission

Aerospace science and technology, 2012-12, Vol.23 (1), p.469-478

2012

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Advanced GNC-oriented modeling and simulation of Vertical Landing vehicles with fuel slosh dynamics

Acta astronautica, 2023-03, Vol.204, p.294-306

2023

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Simulations and Flight Tests of a New Nonlinear Controller for the EAGLE Lander

Journal of spacecraft and rockets, 2019-01, Vol.56 (1), p.259-272

2019

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Using an UAV for testing an autonomous terrain-based optical navigation system for lunar landing

2018 IEEE Aerospace Conference, 2018, p.1-9

2018

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Multiple beacons for supporting lunar landing navigation

CEAS space journal, 2018-09, Vol.10 (3), p.295-305

2018

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Multiple spacecraft configuration designs for coordinated flight missions

CEAS space journal, 2018-06, Vol.10 (2), p.251-271

2018

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Lunar landing navigation supported by ranging to an orbiter

CEAS space journal, 2018-09, Vol.10 (3), p.427-440

2018

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Physical modeling and simulation of electro-mechanical actuator-based TVC systems for reusable launch vehicles

Acta astronautica, 2024-01, Vol.214, p.790-808

2024

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Beacons for supporting lunar landing navigation

CEAS space journal, 2017-03, Vol.9 (1), p.77-95

2017

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Introduction

Space science reviews, 2010-03, Vol.151 (1-3), p.1-3

Theil, Stephan

2010

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Introduction

Space science reviews, 2010-03, Vol.151 (1-3), p.1

Theil, Stephan

2010

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Introduction

Space science reviews, 2010, Vol.151 (1-3), p.1-3

Theil, Stephan

2010

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Architectural elements of hybrid navigation systems for future space transportation

CEAS space journal, 2018-06, Vol.10 (2), p.231-250

2018

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Geostationary Satellite Station-Keeping Using Convex Optimization

Journal of guidance, control, and dynamics, 2016-03, Vol.39 (3), p.605-616

2016

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Quasi-impulsive maneuvers to correct mean orbital elements in LEO

CEAS space journal, 2019-09, Vol.11 (3), p.287-299

2019

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Collocation of Geostationary Satellites Using Convex Optimization

Journal of guidance, control, and dynamics, 2016-06, Vol.39 (6), p.1303-1313

2016

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Robust Tightly Coupled Hybrid Navigation for Space Transportation

Journal of spacecraft and rockets, 2019-03, Vol.56 (2), p.596-609

2019

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Modelling the Attitude Noise of the Gaia Spacecraft. ASimplified Approach

Space science reviews, 2010-03, Vol.151 (1-3), p.197-207

2010

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Modelling the Attitude Noise of the Gaia Spacecraft. A Simplified Approach: Satellite Dynamics : Modelling, In-Orbit Calibration and Data Processing

Space science reviews, 2010, Vol.151 (1-3), p.197-207

2010

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Adaptive Disturbance-Based High-Order Sliding-Mode Control for Hypersonic-Entry Vehicles

Autonomous Trajectory Planning and Guidance Control for Launch Vehicles

Survey of autonomous guidance methods for powered planetary landing

Modeling of a Tethered Testbed for a VTVL Vehicle

Onboard Trajectory Generation for Entry Vehicles via Adaptive Multivariate Pseudospectral Interpolation

Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex–Concave Decomposition

Development of a low cost star tracker for the SHEFEX mission

Advanced GNC-oriented modeling and simulation of Vertical Landing vehicles with fuel slosh dynamics

Simulations and Flight Tests of a New Nonlinear Controller for the EAGLE Lander

Using an UAV for testing an autonomous terrain-based optical navigation system for lunar landing

Multiple beacons for supporting lunar landing navigation

Multiple spacecraft configuration designs for coordinated flight missions

Lunar landing navigation supported by ranging to an orbiter

Physical modeling and simulation of electro-mechanical actuator-based TVC systems for reusable launch vehicles

Beacons for supporting lunar landing navigation

Introduction

Introduction

Introduction

Architectural elements of hybrid navigation systems for future space transportation

Geostationary Satellite Station-Keeping Using Convex Optimization

Quasi-impulsive maneuvers to correct mean orbital elements in LEO

Collocation of Geostationary Satellites Using Convex Optimization

Robust Tightly Coupled Hybrid Navigation for Space Transportation

Modelling the Attitude Noise of the Gaia Spacecraft. ASimplified Approach

Modelling the Attitude Noise of the Gaia Spacecraft. A Simplified Approach: Satellite Dynamics : Modelling, In-Orbit Calibration and Data Processing

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