Paper information
- Paper code
- Date
2016-09-27
- Time
11:30
- Order
7
- Room
Salon de Eventos 1
- Title
Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, thrusters, and piezoelectric transducers as sensors and actuators.
- abstract
- Session
2. Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)
- symposium
C2. MATERIALS AND STRUCTURES SYMPOSIUM
- congress
IAC-16
- Type of presentation
oral
Dr. Ijar M. Da Fonseca, ITA-DCTA, Brazil
Prof. Domingos Rade, Brazil;
Mr. Rodrigo Chales, ITA-DCTA, Brazil;