TY  - JOUR
N1  - cited By 0; Conference of 4th International Conference on Mechanical and Manufacturing Engineering, ICME 2013 ; Conference Date: 17 December 2013 Through 18 December 2013; Conference Code:101955
SP  - 337
TI  - Spin-off maneuvers of flexible satellite using PD based constant - Amplitude inputs
AV  - none
EP  - 344
SN  - 16609336
N2  - Spin-off maneuver of a flexible satellite using constant-amplitude thrusters is studied in this paper. The satellite consists of a rigid main body and two symmetrical solar panels. The panels are having structural flexibility and their motions are discretized following the finite element method. Under constant-amplitude thrusts, steady-state attitude angle oscillations may occur in large amplitude after the maneuvers. Since in operation the satellite should point to certain area on the earth precisely, these oscillations of course are not acceptable. To reduce the oscillations, proportional derivative (PD) based constant-amplitude input shaping logic is proposed to determine time locations of thruster switching. Then, under such inputs, spin-downs of the satellite are simulated numerically. Results of simulations indicate that the precise orientation of the satellite can be achieved. © (2014) Trans Tech Publications, Switzerland.
ID  - scholars4427
KW  - Attitude angle; Constant-amplitude; Flexible satellites; Large amplitude; PD control; Proportional derivatives; Spin-off maneuver; Structural flexibilities
KW  -  Computer control systems; Flexible structures; Industrial engineering; Satellites
KW  -  Amplitude modulation
CY  - Bangi-Putrajaya
A1  - Setyamartana, P.
A1  - Razali, R.
A1  - Zainuddin, A.
JF  - Applied Mechanics and Materials
UR  - https://www.scopus.com/inward/record.uri?eid=2-s2.0-84891929531&doi=10.4028%2fwww.scientific.net%2fAMM.465-466.337&partnerID=40&md5=26f6ef72706b1c49ada6143193ed2145
VL  - 465-46
Y1  - 2014///
ER  -