Author

Seid H Pourtakdoust

Sharif University of Technology - Cited by 1,421 - Professor - Division of Flight Dynamics and Control

Biography

Dr.Seid H Pourtakdoust has done his Ph.D. in Aerospace Engineering,1989, MSc in Aerospace Engineering, 1984, BSc in Aerospace Engineering, 1982. BSc in Civil Engineering, University of Kansas ,USA, 1982. His research interest and activities includes Stochastic Optimal Control, Spacecraft Trajectory Design and Optimization, Aerospace Flight Dynamics, Statistical Analysis/Simulation of Dynamic Systems, Aeroelastic Simulation of Air Vehicles, and Reliability Based Design and Optimization.
Title
Cited by
Year
Advanced UAV aerodynamics, flight stability and control: novel concepts, theory and applications
P Marqués, A Da RonchJohn Wiley & Sons, 2017201
46
2017
Multisensor attitude estimation: fundamental concepts and applications
H Fourati, DEC BelkhiatCRC Press, 2016201
45
2016
Consistent calibration of magnetometers for nonlinear attitude determination
M Kiani, SH Pourtakdoust, AA Sheikhymeasurement 73, 180-190, 2015201
34
2015
State estimation of nonlinear dynamic systems using weighted variance-based adaptive particle swarm optimization
M Kiani, SH PourtakdoustApplied Soft Computing 34, 1-17, 2015201
29
2015
Development of a radiation based heat model for satellite attitude determination
A Labibian, SH Pourtakdoust, A Alikhani, H FouratiAerospace Science and Technology 82, 479-486, 2018201
24
2018
Multidisciplinary design of a guided flying vehicle using simplex nondominated sorting genetic algorithm II
SM Zandavi, SH PourtakdoustStructural and Multidisciplinary Optimization 57, 705-720, 2018201
17
2018
Autonomous temperature-based orbit estimation
FN Gourabi, M Kiani, SH PourtakdoustAerospace Science and Technology 86, 671-682, 2019201
14
2019
Attitude estimation and control based on modified unscented Kalman filter for gyro-less satellite with faulty sensors
SH Pourtakdoust, MF Mehrjardi, MH HajkarimActa Astronautica 191, 4-147, 2021202
13
2021
Performance of a novel heat based model for spacecraft attitude estimation
A Labibian, A Alikhani, SH PourtakdoustAerospace Science and Technology 70, 317-327, 2017201
13
2017
Adaptive square-root cubature–quadrature Kalman particle filter via KLD-sampling for orbit determination
M Kiani, SH PourtakdoustAerospace Science and Technology 46, 159-167, 2015201
13
2015
Utility of probability density evolution method for experimental reliability‐based active vibration control
S Saraygord Afshari, SH PourtakdoustStructural Control and Health Monitoring 25 (8), e2199, 2018201
12
2018
A hybrid simplex non-dominated sorting genetic algorithm for multi-objective optimization
SH Pourtakdoust, SM ZandaviInternational Journal of Swarm Intelligence & Evolutionary Computation 5 (3 …, 2016201
12
2016
Experimental validation of a novel radiation based model for spacecraft attitude estimation
A Labibian, SH Pourtakdoust, M Kiani, AA Sheikhi, A AlikhaniSensors and Actuators A: Physical 250, 4-122, 2016201
11
2016
Reliability analysis of composite anisogrid lattice interstage structure
N Raouf, A Davar, SH PourtakdoustMechanics based design of structures and machines 50 (9), 3322-3330, 2020202
10
2020
Probability density evolution for time-varying reliability assessment of wing structures
SS Afshari, SH PourtakdoustAviation 22 (2), 45-54, 2018201
10
2018
Structural reliability analysis of solid rocket motor with ellipsoidal cap
N Raouf, SH Pourtakdoust, B Ashouri Amin Abadi, A Rajabi-GhanaviehJournal of Spacecraft and Rockets 53 (2), 38-32, 2016201
9
2016
Entropy-based adaptive attitude estimation
M Kiani, A Barzegar, SH PourtakdoustActa Astronautica 144, 271-22, 20120
8
2018
Optimal control of human‐like musculoskeletal arm: Prediction of trajectory and muscle forces
M Sharifi, SH Pourtakdoust, M ParnianpourOptimal Control Applications and Methods 3 (2), 167-13, 2017201
8
2017
Covariance-based multiple-impulse rendezvous design
A Shakouri, M Kiani, SH PourtakdoustIEEE Transactions on Aerospace and Electronic Systems 55 (5), 212-2137, 20120
8
2018
A new shape-based multiple-impulse strategy for coplanar orbital maneuvers
A Shakouri, M Kiani, SH PourtakdoustActa Astronautica 161, 200-20, 2019201
8
2019

Referred From: https://scholar.google.com/citations?user=-Ma0A1wAAAAJ&hl=en

Cited by
Citations 1421
h-index 20
i10-index 43
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