Guidance and control for satellite in-orbit-self-assembly proximity operations
In this paper, the autonomous in-orbit-self-assembly of multiple satellites is exploited in close proximity operations. Guidance and control algorithms are developed based on the closed-form analytical solution of relative motion equations that is completely explicit in time in a general Keplerian o...
| Main Authors: | Okasha, Mohamed Elsayed Aly Abd Elaziz, Park, Chandeok, Park, Sang-Young |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Elsevier Masson SAS
2015
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/41283/ http://irep.iium.edu.my/41283/1/1-s2.0-S1270963814002569-main.pdf |
Similar Items
Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2014)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2014)
Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015)
Satellite orbit and attitude simulator: design and implementation
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
Satellite attitude tracking control using Lyapunov control theory
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2019)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2019)
Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
Autonomous multi satellites assembly in keplerian orbits
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
Magnetic torque attitude control of a satellite using the state-dependent Riccati equation technique
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach
by: Abdelrahman, Mohammad, et al.
Published: (2011)
by: Abdelrahman, Mohammad, et al.
Published: (2011)
A Model Predictive Control (MPC) approach on unit quaternion orientation based quadrotor for trajectory tracking
by: Maidul, Isla, et al.
Published: (2019)
by: Maidul, Isla, et al.
Published: (2019)
Relative motion modeling and control in a perturbed orbit
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2011)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2011)
Low earth orbit design for remote sensing applications
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)
Sigma-point Kalman filtering for spacecraft attitude and rate estimation using magnetometer measurements
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
Integrated attitude determination and control system via magnetic measurements and actuation
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)
Modelling of transversal crack and delamination under traction with XFEM
by: Abdullah, Nur Azam, et al.
Published: (2017)
by: Abdullah, Nur Azam, et al.
Published: (2017)
Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method
by: Abdullah, Nur Azam, et al.
Published: (2017)
by: Abdullah, Nur Azam, et al.
Published: (2017)
Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)
by: Abdullah, Nur Azam, et al.
Published: (2018)
Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM
by: Abdullah, Nur Azam, et al.
Published: (2018)
by: Abdullah, Nur Azam, et al.
Published: (2018)
Quadrotor trajectory tracking using PID cascade control
by: Idres, Moumen, et al.
Published: (2017)
by: Idres, Moumen, et al.
Published: (2017)
Performance evaluation of linear quadratic regulator and linear quadratic Gaussian controllers on quadrotor platform
by: Islam, Maidul, et al.
Published: (2019)
by: Islam, Maidul, et al.
Published: (2019)
New algorithm for attitude and orbit determination using magnetic field measurements
by: Abdelrahman, Mohammad
Published: (2015)
by: Abdelrahman, Mohammad
Published: (2015)
Satellite attitude tracking control using thrusters and momentum wheels
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
Effect of level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2016)
by: Quadros, Jaimon Dennis, et al.
Published: (2016)
ESA 380/3 ORBITAL MECHANICS [MEKANIK ORBIT] JUNE 2016
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)
Satellite attitude determination utilizing measurement
sensor data and kalman filtering
by: Samaan, Malak A., et al.
Published: (2006)
by: Samaan, Malak A., et al.
Published: (2006)
Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2011)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2011)
Second Semester Examination 2017/2018 Academic Session
May/June 2018 ESA380/3 – Orbital Mechanics [Mekanik Orbit] Duration : 3 hours Masa : 3 jam
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2018)
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2018)
Optimization of driving mode switching strategy for a multimode plug-in hybrid electric vehicle
by: Idres, Moumen, et al.
Published: (2019)
by: Idres, Moumen, et al.
Published: (2019)
DYNAMICS AND CONTROL OF MINI AERIAL VEHICLE USING MODEL PREDICTIVE CONTROL
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
Finite Element Software Development of a Flexible
Satellite Orbiting in Space
by: Parman, Setyamartana
Published: (2009)
by: Parman, Setyamartana
Published: (2009)
Evaluation performance of linear quadratic regulator and linear quadratic gaussian controllers on quadrotor platform
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)
Optimization of driving mode switching strategy for a multimode plug-in hybrid electric vehicle
by: Idres, Moumen, et al.
Published: (2019)
by: Idres, Moumen, et al.
Published: (2019)
Studies on suddenly expanded flow at different levels of over expansion for area ratio 3.24
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Wall pressure studies in a suddenly expanded flow for area ratio 2.56”
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
High incidence supersonic similitude for planar wedge
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Estimation of stability derivatives of a delta wing in hypersonic flow
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Oscillating supersonic delta wings with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Effect on base pressure in suddenly expanded flows with variable location of microjets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Experimental studies on low speed converging nozzle flow with sudden expansion
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
ESA 380 – ORBITAL MECHANICS JANUARY 2014
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)
Similar Items
-
Guidance, navigation and control for satellite proximity operations using Tschauner-Hempel equations
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2014) -
Modeling, dynamics and control of spacecraft relative motion in a perturbed keplerian orbit
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015) -
Satellite orbit and attitude simulator: design and implementation
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013) -
Satellite attitude tracking control using Lyapunov control theory
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2019) -
Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements
by: Mohammad Abdelrahman, Mohammad Ibraheem, et al.
Published: (2011)