Prof. Eng. Tamer Mekky Ahmed Ibrahim Habib

Summary :

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Education :

  • Cairo University.
Faculty of engineering
Aerospace department
  • Master Degree of Science (Awarding year – 2003)
  • Doctor of Philosophy (Awarding year – 2009).

Publications :

1- T.M. Habib, A.H., Kassem, and G. M., El-Bayoumi,“GPS-Based Small Satellite Position and Attitude Determination Simulator”, Journal of Engineering and Applied Science, Vol. 52, No. 1,2005, pp. 71-87.
2- T.M. Habib, S.D., Hassan, and G. M., El-Bayoumi, “Spacecraft Attitude and Attitude Rate Estimation Using Hybrid Kalman Filtering of Magnetometer Measurements”, Proceeding of the 12-th International Conference on Aerospace science and Aviation Technology, 2007.
3- T.M. Habib, “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”, The Egyptian Journal of Remote Sensing and Space Sciences, Vol.14, Issue 2, Dec.2011, pp. 57-61.
4- T.M. Habib, “Global Optimum Spacecraft Orbit Control Subject to Bounded Thrust in Presence of Nonlinear and Random Disturbances in a Low Earth Orbit”, The Egyptian Journal of Remote Sensing and Space Sciences, Vol.15,Issue 1, June, 2012, pp. 1-8.
5- T.M. Habib, “Innovative Airborne and Aerospace Solutions for Defense and Remote-sensing”, The First International Conference on New Trends and Applications of GNSS, Cairo University, 2012.
6- T.M. Habib, “A Comparative Study of Spacecraft Attitude Determination and Estimation Algorithms( A costbenefit approach)”, Aerospace Science and Technology, Vol.26, Issue 1, April-May, 2013, pp. 211-215.
7- T.M. Habib, “Simultaneous spacecraft orbit estimation and control based on GPS measurements via extended Kalman filter”, The Egyptian Journal of Remote Sensing and Space Sciences, Vol.16, Issue 1, 2013, pp. 11-16.
8- T.M. Habib, “Concurrent Spacecraft Attitude and Orbit Estimation with Attitude Control Based on Magnetometer,Gyroscope, and GPS Measurements through Extended Kalman Filter”,Journal of Basic and Applied Sciences, Vol. 10, 2014, pp. 461-468.
9- T.M. Habib, “Artificial Satellites: History, Future, and Precautions”, Science, Vol.444, 2013, pp. 38-39.
10- T.M. Habib, “Combined Spacecraft Orbit and Attitude Control Through Extended Kalman Filtering of Magnetometer, Gyro, and GPS Measurements”, The Egyptian Journal of Remote Sensing and Space Sciences,Vol.17, Issue 1, Jan, 2014, pp. 87-94.
11- M., Awad, M., Mahmoud, T., Habib, , A., Mohamed, “Prediction of the orbital motion of an artificial satellite from radar measurements”, Al Azhar Bulletin of Science - Basic Science Sector, Vol.25, No. 1, June, 2014, pp. 15-20.
12- T.M. Habib, “A Review and a Quantitative Comparison among the Exact Solution and the Numerical Integration Methods with Fixed Time Step Commonly Used to Solve the Two-Body Problem”, Proceeding of the 7-th International Conference on Mathematics and Engineering Physics, May, 2014.
13- T.M. Habib, “Egyptsat; An Integrated Road Map for Suggested Research Points – Astrodynamics Perspective”, ISNET/TUBITAK UZAY Workshop on Small Satellite Engineering and Design for OIC Countries, Oct, 2014.
14- T.M. Habib, “Necessary modifications to the strapdown inertial navigation system model for non-earth-based users”, International Journal of Aeronautical Science & Aerospace Research,2015, 3, pp.1-11.
15- T.M. Habib, K.A., Kamalaldin, and A.H. Kassem “Commercial Cameras Accurate Focal Length Estimation for Satellite Optical Observation”, International Journal of Aeronautical Science & Aerospace Research,2015, 2(4),pp.39-47.
16- A. H, Kassem, G. M. , El-bayoumi, T.M, Habib,and K.A., Kamalaldin, “Improving Satellite Orbit Estimation using Commercial Cameras”, International Review of Aerospace Engineering, Vol.8, No. 5, Oct., 2015, pp. 174-178.
17- T.M. Habib, “A New Optimal Fusion Algorithm for Spacecraft Attitude Determination and Estimation Algorithms”, The Egyptian Journal of Remote Sensing and Space Sciences, Vol.21, 2018, pp. 305-309.
18- T.M, Habib, “In-Orbit Spacecraft Inertia, Attitude, and Orbit Estimation Based on Measurements of Magnetometer, Gyro, Star Sensor, and GPS Through Extended Kalman Filter”, International Review of Aerospace Engineering,Vol.11, No. 6, Dec., 2018, pp. 247-251.
19- T.M, Habib, “Spacecraft Nonlinear Attitude Dynamics Control with Adaptive Neuro-Fuzzy Inference System”, International Review of Automatic Control, Vol.12, No. 5, Dec., 2019, pp. 242-250.