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Microprocessor controlled force actuator
- Source :
- Journal of Guidance, Control, and Dynamics. 11:230-236
- Publication Year :
- 1988
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 1988.
-
Abstract
- The mechanical and electrical design of a prototype force actuator for vibration control of large space structures (LSS) is described. The force actuator is an electromagnetic system that produces a force by reacting against a proof-mass. The actuator has two colocated sensors, a digital microcontroller, and a power amplifier. The total weight of actuator is .998 kg. The actuator has a steady state force output of approximately 2.75 N from approximately 2 Hz to well beyond 1000 Hz.
- Subjects :
- Physics
Steady state (electronics)
Cantilever
Pneumatic actuator
Applied Mathematics
Amplifier
Vibration control
Aerospace Engineering
law.invention
Computer Science::Other
Computer Science::Robotics
Microprocessor
Microcontroller
law
Computer Science::Systems and Control
Space and Planetary Science
Control and Systems Engineering
Electromagnetism
Control theory
Active vibration control
Electromagnetic system
Electrical and Electronic Engineering
Actuator
Subjects
Details
- ISSN :
- 15333884 and 07315090
- Volume :
- 11
- Database :
- OpenAIRE
- Journal :
- Journal of Guidance, Control, and Dynamics
- Accession number :
- edsair.doi.dedup.....b64add3ac3c4d45b6bb84dcf5689dc7a