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Mohammad Reza Mortazavi
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Year
Pitch and flight path controller design for F-16 aircraft using combination of LQR and EA techniques
MR Mortazavi, A Naghash
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2018
92018
Optimal midcourse guidance of an air-to-air missile via SVM and RVM
MR Mortazavi, F Almasganj
Soft Computing 23 (15), 6603-6616, 2019
72019
A probabilistic approach to classification of human performance during interaction with a standard flight tasks simulator
MR Mortazavi, K Raissi, SHH Mehne
Journal of Ambient Intelligence and Humanized Computing 10 (8), 3211-3230, 2019
52019
Pilot workload assessment under different levels of autopilot failure
MR Mortazavi, K Raissi, SH Hashemi Mehne
Scientia Iranica 26 (Special Issue on: Socio-Cognitive Engine), 114-126, 2019
12019
Creating a Numerical Index for Measurement of Workload Levels in the Simulator of Piloting Tasks (in Persian)
MR Mortazavi, K Raissi, SH Hashemi
Iranian Journal of Ergonomics 4 (4), 24-32, 2017
1*2017
Identification of Aircraft Dynamic Model Using Artificial Neural Networks (in Persian)
MR Mortazavi, M Mortazavi
Aerospace Knowledge and Technology Journal 1 (2), 15-23, 2012
1*2012
Mathematical modeling of human-machine interaction in multi attribute piloting tasks simulator using information theory (in Persian)
SHHM Mohammad Reza Mortazavi, Kamran Raissi
Aerospace Knowledge and Technology Journal 8 (2), 153-167, 2019
2019
An investigation of Vitamin D effect on alterations of glomerular filtration rate (GFR) in patients with chronic renal failure
S Boya, SM Hashemi, M Mortazavi
Der Pharmacia Lettre 8 (8), 221-226, 2016
2016
Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation (in Persian)
MR Mortazavi, A Alireza
Journal of Space Science and Techonlogy 8 (1), 27-41, 2014
2014
Creating desired eigenstructure for longitudinal stabilizer of a fighter aircraft via linear quadratic regulator (in Persian)
MR Mortazavi, A Naghash
The 13th Conference of Iranian Aerospace Society, Tehran, Iran, 2014
2014
A New Approach to Design an Optimum Launch Window for a Sample Micro-Satellite
MS Mohammadi, M Mortazavi, M Malekan
Space Science and Technology 6 (4), 43-52, 2014
2014
Indirect robust control of spacecraft based on θ-D method as a optimal control approach (in Persian)
MR Mortazavi, K Raissi
The 3rd International Conference on Control, Instrumentation and Automation …, 2013
2013
Aircraft system identification by means of neural networks and fuzzy logic (in Persian)
MR Mortazavi, M Mortazavi, K Raissi
The 10th Conference of Iranian Aerospace Society, Tehran, Iran, 2011
2011
Flight parameters estimation via neural networks (in Persian)
MR Mortazavi, M Mortazavi, K Raissi
The 10th Conference of Iranian Aerospace Society, Tehran, Iran, 2011
2011
Modelling 6DOF dynamic of an airplane using artificial neural networks (in Persian)
MR Mortazavi, M Mortazavi
The 9th Conference of Iranian Aerospace Society, Tehran, Iran, 2010
2010
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