Finite Element Software Development of a Flexible
Satellite Orbiting in Space

QR Code

Finite Element Software Development of a Flexible Satellite Orbiting in Space

A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For...

Full description

Bibliographic Details
Main Author:	Parman, Setyamartana
Format:	Conference or Workshop Item
Language:	English
Published:	2009
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://scholars.utp.edu.my/id/eprint/1089/ http://scholars.utp.edu.my/id/eprint/1089/1/75-59916-review.pdf

Similar Items

Controlling Attitude Maneuvers of a Flexible Satellite under Low Frequency Vibration by Using Feed-Forward Constant-Amplitude Inputs
by: Parman, Setyamartana
Published: (2008)

Attitude Control of Flexible System by Shaping Constant-Amplitude Input
by: Ibrahim, Idris, et al.
Published: (2008)

Attitude Control of Linear System by Using Feed- Forward Constant-Amplitude Inputs
by: Parman, Setyamartana
Published: (2008)

Finite element analysis of automotive intake manifold using CAE software
by: Muhammad Haikal, Haron
Published: (2008)

Relative motion modeling and control in a perturbed orbit
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2011)

Finite element analysis of cam and its follower contact stress mechanism
by: Mohd Hafiz, Ghazalli
Published: (2007)

Finite element stress analysis on natural gas motorcycle intake manifold
by: Yaacob, Zulkefli, et al.
Published: (2008)

Low earth orbit design for remote sensing applications
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2013)

Simulation stress and finite element analysis based of Suzuki FXR 150cc motorcycle chassis
by: Mohd Khairudin, Yahya
Published: (2007)

The effect of modal properties of crash box structures with trigger mechanisms towards the crashworthiness by using finite element analysis
by: Asri, M. N. A. M., et al.
Published: (2021)

Satellite attitude tracking control using thrusters and momentum wheels
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2018)

ESA 380/3 ORBITAL MECHANICS [MEKANIK ORBIT] JUNE 2016
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)

Satellite synthetic aperture radar (SAR) coastal water backcatter study
by: Marghany, Maged Mahmoud
Published: (2008)

Development of four wheels space-frame hybrid air motorcycle chassis
by: Ser, Beng Sian
Published: (2013)

Development of two wheels space-frame plug-in hybrid electric motorcycle chassis
by: Muhammad Akmal, Jamaludin
Published: (2013)

Vibration suppression of flexible beam using eddy current damper
by: Hasan, Zainal Abidin
Published: (2013)

Vibration suppression of flexible beam using electromagnetic shunt damper
by: Ariffin, Abdullah
Published: (2013)

Software development for aerodynamic characteristics estimation of wing-body combination of aircraft at cubsonic speeds
by: Dahalan, Md. Nizam, et al.
Published: (2001)

ESA 380/3 - ORBITAL MECHANICS NOV 09.
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2009)

ESA 380/3 – ORBITAL MECHANICS NOV 2010.
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2010)

Flexible valve timing strategies for boosting a small four-stroke spark ignition engine performance
by: Mohd Razali, Hanipah, et al.
Published: (2020)

Application of the aerodynamic discrete element methods
by: Sulaeman, Erwin
Published: (2011)

Satellite attitude tracking control using Lyapunov control theory
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2019)

Power Subsystem Design Of The Malaysian Youth Satellite (Mysat)
by: Subramaniam, Sasidaran
Published: (2018)

A fitting farewell gift for Dr Mahathir as we soar into space
by: Abd Razak, Dzulkifli
Published: (2003)

Educational software for stress analysis of idealized closed thin walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)

Educational software for stress analysis of non-idealized closed thin-walled sections
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2018)

Simulation test of automotive intake valve using computer aided engineering software
by: Hafierul Hafiz, Md Razi
Published: (2008)

Simulation test of automotive alloy wheel using computer aided engineering software
by: Mohd Izzat Faliqfarhan, Baharom
Published: (2008)

ESA380/3 ORBITAL MECHANICS JUN 2015)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2016)

Guidance and control for satellite in-orbit-self-assembly proximity operations
by: Okasha, Mohamed Elsayed Aly Abd Elaziz, et al.
Published: (2015)

Active Learning In Satellite Mission Design
by: Mohd Dahlan, Siti Fariza, et al.
Published: (2004)

The Application of Combined Momentum â€“ Blade Element Theory for Aerodynamics Analysis Helicopter Rotor Blade in the Forward Flight
by: Ghazirah, Ghazirah, et al.
Published: (2006)

An Active Force Control (Afc) Based Control Momen Gyros for Attitude Control of Small Satellite
by: Salleh, Mohd Badrul
Published: (2016)

A matlab based educational software for the study on the effect of cut-out in aircraft wings
by: Mohammed Riyadh, Miah, et al.
Published: (2018)

Finite element modeling and updating of the composite plate structure
by: R. M., Yaacob, et al.
Published: (2019)

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)

An optimum magnetic control torque generation of a momentum bias satellite
by: Mohd Suhadis, Nurulasikin, et al.
Published: (2014)

An optimum magnetic control torque generation of a momentum bias satellite
by: Mohd Suhadis, Nurulasikin, et al.
Published: (2014)

The Preliminary Design Of A Nano Satellite Engineering Model For Remote Sensing Expe
by: Md. Said, Md. Azlin, et al.
Published: (2003)

Cannot write session to /tmp/vufind_sessions/sess_jb757br7a9mokvknipmgvln6n0