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Tamer Mekky Ahmed Habib
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Cited by
Cited by
Year
A comparative study of spacecraft attitude determination and estimation algorithms (a cost–benefit approach)
TMA Habib
Aerospace Science and Technology 26 (1), 211-215, 2013
272013
Simultaneous spacecraft orbit estimation and control based on GPS measurements via extended Kalman filter
TMA Habib
The Egyptian Journal of Remote Sensing and Space Science 16 (1), 11-16, 2013
142013
New algorithms of nonlinear spacecraft attitude control via attitude, angular velocity, and orbit estimation based on the Earth’s magnetic field
M Tamer
Ph. D. Thesis, Cairo University, 2009
112009
Fast converging with high accuracy estimates of satellite attitude and orbit based on magnetometer augmented with gyro, star sensor and GPS via extended Kalman filter
TMA Habib
The Egyptian Journal of Remote Sensing and Space Science 14 (2), 57-61, 2011
102011
The global positioning system application to satellite position and attitude determination
M Tamer
M. Sc. thesis, Aerospace Department, Cairo University, 2003
92003
Artificial Intelligence for Spacecraft Guidance, Navigation, and Control: A state-of-the-art
TMA Habib
Aerospace Systems, 2022
82022
A new optimal fusion algorithm for spacecraft attitude determination and estimation algorithms
TMA Habib
The Egyptian Journal of Remote Sensing and Space Science, 2017
72017
Combined spacecraft orbit and attitude control through extended Kalman filtering of magnetometer, gyro, and GPS measurements
TMA Habib
The Egyptian Journal of Remote Sensing and Space Science 17 (1), 87-94, 2014
72014
Global optimum spacecraft orbit control subject to bounded thrust in presence of nonlinear and random disturbances in a low earth orbit
TMA Habib
The Egyptian Journal of Remote Sensing and Space Science 15 (1), 1-8, 2012
52012
Efficient Simultaneous Spacecraft Attitude and Orbit Estimation via Neural Networks
A T.M, Habib, and R.
International Review of Aerospace Engineering 14 (6), 346-353, 2021
42021
Replacement of In-Orbit Modern Spacecraft Attitude Determination and Estimation Algorithms with Neural Networks
TMA Habib
International Review of Aerospace Engineering 14 (3), 166-172, 2021
42021
In-Orbit Spacecraft Inertia, Attitude, and Orbit Estimation Based on Measurements of Magnetometer, Gyro, Star Sensor and GPS Through Extended Kalman Filter,(2018)
TM Habib
International Review of Aerospace Engineering (IREASE) 11 (6), 247-251, 2018
42018
Modelling of Spacecraft Orbit via Neural Networks
A T.M, Habib, and R.
International Review of Aerospace Engineering 14 (5), 285-293, 2021
32021
Spacecraft Attitude and Orbit Determination from the Cost and Reliability Viewpoint: A Review
H T.M
ASRIC Journal on Natural Sciences 1, 14-35, 2022
22022
Replacement of In-Orbit Spacecraft Attitude Determination Algorithms with Adaptive Neuro-Fuzzy Inference System via Subtractive Clustering
A T.M., Habib, and R.
International Review of Aerospace Engineering 14 (4), 220-227, 2021
22021
Replacement of In-Orbit Extended Kalman Filter for Spacecraft Orbit Estimation via Neural Networks
H T.M
International Review of Automatic Control 14 (4), 224-232, 2021
22021
In-Orbit Three-Axis Spacecraft Orbit Control Based on Neural Networks via Limited Thrust Budget
RAA Tamer Mekky Habib
International Review of Automatic Control 14 (3), 144-152, 2021
22021
Nonlinear Spacecraft Attitude Control via Cascade-Forward Neural Networks
TMA Habib
International Review of Automatic Control 13 (3), 146-152, 2020
22020
Spacecraft Nonlinear Attitude Dynamics Control with Adaptive Neuro-Fuzzy Inference System
TMA Habib
International Review of Automatic Control 12 (5), 242-250, 2019
22019
Concurrent spacecraft attitude and orbit estimation with attitude control based on magnetometer, gyroscope, and GPS measurements through extended Kalman filter
TM Habib
International Conference on Aerospace Sciences and Aviation Technology 15 …, 2013
22013
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