New algorithm for attitude and orbit determination using magnetic field measurements
A generalized algorithm for a Combined Nonlinear Control and Estimation CNCE process for spacecraft attitude and orbit determination and control is pre-sented. The approach tends to eliminate the delays due to the separation be-tween the estimation and control processes. Also, it minimizes the possi...
| Main Author: | Abdelrahman, Mohammad |
|---|---|
| Format: | Proceeding Paper |
| Language: | English English |
| Published: |
2015
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/41652/ http://irep.iium.edu.my/41652/1/AAS_15-405_web.pdf http://irep.iium.edu.my/41652/4/SFM2015_Conference_Program_Final.pdf |
Similar Items
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)
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)
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)
Spacecraft sun-pointing using coplanar solar panels data and magnetic field measurements
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2013)
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2013)
Spacecraft attitude control: development and application of new algorithms
by: Abdelrahman, Mohammad, et al.
Published: (2012)
by: Abdelrahman, Mohammad, et al.
Published: (2012)
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)
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)
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)
New algorithm for gyroless spacecraft angular rate Estimation and its application
by: Abdelrahman, Mohammad, et al.
Published: (2006)
by: Abdelrahman, Mohammad, et al.
Published: (2006)
Multi-Object Attitude and Rate Tracking for Spacecraft in
Formation Flying
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem
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)
Space vehicles dynamics and control
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2011)
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2011)
Developing magnetic damper system for microsatellite
by: Legowo, Ari, et al.
Published: (2019)
by: Legowo, Ari, et al.
Published: (2019)
Adaptive neuro-fuzzy control approach for spacecraft maneuvers
by: Abdelrahman, Mohammad, et al.
Published: (2006)
by: Abdelrahman, Mohammad, et al.
Published: (2006)
Guidance and control for satellite in-orbit-self-assembly proximity operations
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015)
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015)
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)
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)
UNIVERSITI SAINS MALAYSIA First Semester Examination
2012/2013 Academic Session January 2013 ESA 380/3 – Orbital Mechanics [Mekanik Orbit] Duration : 3 hours
[Masa: 3 jam]
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
UNIVERSITI SAINS MALAYSIA Second Semester Examination
2012/2013 Academic Session June 2013 ESA 380/3 – Orbital Mechanics [Mekanik Orbit] Duration : 3 hours [Masa: 3 jam]
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
by: Aeroangkasa, Pusat Pengajian Kejuruteraan
Published: (2013)
CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
by: Khan, Ambareen, et al.
Published: (2018)
by: Khan, Ambareen, et al.
Published: (2018)
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)
An effect of sweep angle on roll damping derivative for a
Delta wing with curved leading edges in unsteady flow
by: Monis, Renita Sharon, et al.
Published: (2019)
by: Monis, Renita Sharon, et al.
Published: (2019)
An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle
by: Khan, Sher Afghan, et al.
Published: (2016)
by: Khan, Sher Afghan, et al.
Published: (2016)
The effect of micro jets on wall pressure for sonic under expanded flow
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Studies on wall pressure of sonic flow through the converging nozzles for different area ratios
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Hypersonic similitude for planar wedges
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Estimation of stability derivatives for a planar wedge in the newtonian limit
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Effect of angle of incidence on roll damping derivatives of a delta wing
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Effect of angle of incidence on stability derivatives of a wing
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Effect of area ratio on base pressure and control effectiveness
by: G. M., Fharukh Ahmed, et al.
Published: (2019)
by: G. M., Fharukh Ahmed, et al.
Published: (2019)
Assessment of different turbulence models in simulating
axisymmetric flow in suddenly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow
by: SHAMITHA, A, et al.
Published: (2020)
by: SHAMITHA, A, et al.
Published: (2020)
Al-Zarqali on instrumentation
by: Ushama, Imama Karim Manba, et al.
Published: (2011)
by: Ushama, Imama Karim Manba, et al.
Published: (2011)
Ibn al Shatir's influence on modern astronomy
by: Abbas, Phirdaous, et al.
Published: (2011)
by: Abbas, Phirdaous, et al.
Published: (2011)
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)
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)
Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015)
by: Khan, Sher Afghan
Published: (2015)
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2016)
by: Sethuraman, Vigneshvaran, et al.
Published: (2016)
Experimental study of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2016)
by: Khan, Sher Afghan, et al.
Published: (2016)
Similar Items
-
Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements
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) -
Satellite orbit and attitude simulator: design and implementation
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013) -
Spacecraft sun-pointing using coplanar solar panels data and magnetic field measurements
by: Mohammad Abdelrahman, Mohammad Ibraheem
Published: (2013) -
Spacecraft attitude control: development and application of new algorithms
by: Abdelrahman, Mohammad, et al.
Published: (2012)