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Seyed Hussein Sadati

Observed names: S.H. Sadati, Seyed H. Sadati, Seyed Hossein Sadati
ORCID: 0000-0002-3948-3375
Observed ORCIDs: 0000-0002-3948-3375, 0000-0003-4007-6125
OpenAlex ID: A5121903584
Resilient Integrated Guidance and Control for Long‐Range High‐Speed Aerospace Vehicles Using LSTM‐Enhanced ACHSOMC in GNSS‐Denied Environments
2026 · Mohammad Mahdi Soori, Seyed Hossein Sadati · Modelling and Simulation in Engineering · 4
Adaptive Neural‐Augmented High‐Order Sliding Mode Control for Integrated UAV Guidance in Uncertain Environments
2025 · Mohamad Mahdi Soori, Seyed Hossein Sadati · Modelling and Simulation in Engineering · 2
PDF
Adaptive neuro fuzzy sliding mode control for trajectory tracking of a fully actuated quadrotor
2026 · Pedram Kabiri, Seyed Hossein Sadati · Results in Engineering · 1
Adaptive Higher Order Continuous Sliding Mode Integrated Guidance and Control With Neural Disturbance Compensation for Intercepting Maneuvering Targets
2026 · Mohamad Mahdi Soori, Seyed Hossein Sadati · Modelling and Simulation in Engineering · 1
Comparison of Flight Control System Design Methods in Landing
2011 · S.H. Sadati, M.Sabzeh Parvar, et al. · InTech eBooks · 1
PDF
Dynamic Performance Enhancement of a High‐Agility Hypersonic Mechanical System via a Learning‐Augmented Robust Control Architecture
2026 · Mohammad Mahdi Soori, Seyed Hossein Sadati · International journal of mechanical system dynamics
PDF
Integrated Estimation and Control with Modified Adaptive Super-Twisting Algorithm for Highly Maneuverable Airplane Under Sensor Faults and External Disturbances
2026 · Javad Naderifar, Mostafa Khazaee, et al. · International Journal of Aeronautical and Space Sciences
Design and Robust Control of a Fully Actuated UAV With a Tubular Reservoir for Hazardous Liquid Transport
2026 · Pedram Kabiri, Seyed Hossein Sadati · Modelling and Simulation in Engineering
Deep Recurrent‐Augmented Adaptive Sliding Mode Guidance for Hypersonic Vehicles in GNSS‐Denied Environments
2026 · Mohammad Mahdi Soori, Seyed Hossein Sadati · Modelling and Simulation in Engineering
PDF
Design of Flight Control System Based on Nonlinear Dynamic Inversion Controller with Structural Damage in Tail
2025 · Mohsen Rahnama, Seyed Hussein Sadati, et al. · Journal of Aerospace Mechanics
Works count: 10
Citation count: 9
H-index: 2
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