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  1. 1

    Magnetic attitude control options for earth pointing small satellite by Mohd Suhadis, Nurulasikin

    Published 2011
    “…The developed control algorithms are modeled using the MATLAB SIMULINK codes. …”
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    Thesis
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    Spacecraft attitude control: development and application of new algorithms by Abdelrahman, Mohammad, Hassan, Sayed

    Published 2012
    “…The main goal of the research is to collect and develop new attitude algorithms that build up the different scenarios acted by a spacecraft starting from the orbit injection phase. …”
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    Book
  4. 4

    A study of coupled magnetic fields for an optimum torque generation by Mohd Suhadis, Nurulasikin, Varatharajoo, Renuganth

    Published 2012
    “…Their attitude torque generation performances were compared and it is found that the optimum torques can be generated by both the developed control algorithms. …”
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    Article
  5. 5

    Satellite attitude tracking control using thrusters and momentum wheels by Okasha, Mohamed Elsayed Aly Abd Elaziz, Idres, Moumen, Abdul Ghaffar, Alia Farhana

    Published 2018
    “…This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tracking manoeuver. …”
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    Proceeding Paper
  6. 6

    Satellite attitude tracking control using Lyapunov control theory by Okasha, Mohamed Elsayed Aly Abd Elaziz, Idres, Moumen, Ghaffar, Alia

    Published 2019
    “…This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tracking manoeuver. …”
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    Article
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    Space vehicles dynamics and control by Mohammad Abdelrahman, Mohammad Ibraheem

    Published 2011
    “…In both modes the active magnetic control algorithms have been introduced and developed. …”
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  9. 9

    Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations by Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett

    Published 2011
    “…In this paper, the development of relative navigation, guidance, and control algorithms of an autonomous space rendezvous and docking system are presented. …”
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    Proceeding Paper
  10. 10

    Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying by Mohammad Abdelrahman, Mohammad Ibraheem

    Published 2011
    “…The developed controller is adopted to solve a trajectory tracking/ model following problem. …”
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    Proceeding Paper
  11. 11

    Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations by Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett

    Published 2014
    “…In this paper, the development of relative navigation, guidance, and control algorithms of an autonomous space rendezvous and docking system are presented. …”
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    Article
  12. 12

    Enhanced attitude control structure for small satellites with reaction wheels by Ismail, Zuliana

    Published 2019
    “…All the relevant attitude control architectures are developed together with their governing equations. …”
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    Thesis
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    Feedback slew algorithms for prolate spinners using Single–Thruster by Yang, Gao, Abadi, Chanik

    Published 2018
    “…A number of low-cost open-loop slew control algorithms have been developed for prolate spinning spacecraft using single-thruster actuation. …”
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    Article
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    Nano-satellite attitude control system based on adaptive neuro-controller by Sharun, S.M., Mashor, M.Y., W. N., Hadani, M.N., Norhayati, Yaacob, S.

    Published 2011
    “…The current research focuses on designing of an intelligent controller for attitude control system (ACS) of nano-satellite. …”
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    Conference or Workshop Item
  18. 18

    Integrated attitude determination and control system via magnetic measurements and actuation only by Mohammad Abdel Rahman, Mohammad Ibraheem, Sang-Young, Park

    Published 2009
    “…The full-state knowledge, required for the control loop is provided through a generalized algorithm for spacecraft three-axis attitude and rate estimation based on the utilization of magnetometer measurements and their time derivatives, while the control torque is generated via magnetorquers. …”
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    Proceeding Paper
  19. 19

    Integrated attitude determination and control system via magnetic measurements and actuation by Mohammad Abdelrahman, Mohammad Ibraheem, Park, Sang-Young

    Published 2011
    “…The full-state knowledge required for the control loop is provided through a generalized algorithm for spacecraft three-axis attitude and rate estimation based on the utilization of magnetometer measurements and their time derivatives, while the control torque is generated via magnetorquers. …”
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    Article
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