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Seyed Hamid Jalali Naini
Seyed Hamid Jalali Naini
Associate Professor, Tarbiat Modares University
Correu electrònic verificat a modares.ac.ir - Pàgina d'inici
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Robust optimization of satellite attitude control system with on-off thruster under uncertainty
V Bohlouri, M Ebrahimi, SHJ Naini
2017 International Conference on Mechanical, System and Control Engineering …, 2017
142017
Closed-form solution of line-of-sight trajectory for nonmaneuvering targets
SH Jalali-Naini, V Esfahanian
Journal of Guidance, Control, and Dynamics 23 (2), 365-366, 2000
132000
Modern explicit guidance law for high-order dynamics
SH Jalali-Naini
Journal of guidance, control, and dynamics 27 (5), 918-922, 2004
122004
Spacecraft attitude control using model-based disturbance feedback control strategy
V Bohlouri, Z Khodamoradi, SH Jalali-Naini
Journal of the Brazilian Society of Mechanical Sciences and Engineering 40 …, 2018
112018
Analytical study of a modified LOS guidance
S Jalali-Naini
AIAA Guidance, Navigation, and Control Conference and Exhibit, 4045, 2001
92001
Preliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers
SH Jalali-Naini, SA Darani
Journal of Aerospace Science and Technology 11 (1), 2017
82017
Modern midcourse guidance laws in the endoatmosphere
SH Jalali-Naini, SH Pourtakdoust
AIAA Guidance, Navigation, and Control Conference and Exhibit, 6291, 2005
82005
Normalized miss distance analysis of single-lag optimal guidance law with radome e ect, saturation and fth-order control system
SH Jalali-Naini
Scientia Iranica, Transactions B 21 (5), 1683-1692, 2014
7*2014
Application of reliability-based robust optimization in spacecraft attitude control with PWPF modulator under uncertainties
V Bohlouri, SH Jalali-Naini
Journal of the Brazilian Society of Mechanical Sciences and Engineering 41 …, 2019
62019
Second-order optimal line-of-sight guidance for stationary targets
SH Sajjadi, SH Jalali Naini
Modares Mechanical Engineering 15 (11), 387-395, 2016
52016
On the predicted errors of atmospheric guidance laws
SH Jalali-Naini, SH Pourtakdoust
Aircraft Engineering and Aerospace Technology 80 (3), 262-273, 2008
42008
First-order optimal line-of-sight guidance for stationary targets
SH Jalali-Naini, SH Sajjadi
Scientia Iranica. Transaction B, Mechanical Engineering 23 (2), 588, 2016
32016
A Modified Midcourse Guidance Law Based on Generalized Collision Course
NSH JALALI, SH Pourtakdoust
JOURNAL OF AEROSPACE SCIENCE AND TECHNOLOGY (JAST) 3 (3), 113-123, 2006
32006
Generalized line-of-sight guidance with lead angle
SH Jalali-Naini
Iranian Journal of Science and Technology 28 (B4), 489-493, 2004
3*2004
Closed-form solution of 3-D line-of-sight guidance
SH Jalali-Naini, V Esfahanian
Proc. of the First International Conference of the Iranian Aerospace Society …, 0
3
A Modification to Integral Pulse-Width Pulse-Frequency Modulator
SH Jalali Naini, O Omidi Hemmat
Journal of Space Science and Technology 14 (1), 55-64, 2021
22021
Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption
SH Jalali Naini
Journal of Aerospace Science and Technology 9 (2), 2012
22012
Differential Equation of Sensitivity Matrix for Final Velocity Constraint
SH Jalali Naini
Journal of Aerospace Science and Technology 6 (2), 55-61, 2009
22009
Modern Midcourse Guidance Law with High-Order Dynamics
SH Jalali-Naini
AIAA Guidance, Navigation, and Control Conference and Exhibit, 5356, 2003
22003
Solution of Three-Dimensional Line-of-Sight Guidance with a Moving Tracker
SH Jalali-Naini, V Esfahanian
Scientia Iranica 11 (1&2), 138-145, 0
2*
En aquests moments el sistema no pot dur a terme l'operació. Torneu-ho a provar més tard.
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