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Digital control system for space structure dampersA digital controller was developed using an SKD-51 System Design Kit, which incorporates an 8031 microcontroller. The necessary interfaces were installed in the wire wrap area of the SKD-51 and a pulse width modulator was developed to drive the coil of the actuator. Also, control equations were developed, using floating-point arithmetic. The design of the digital control system is emphasized, and it is shown that, provided certain rules are followed, an adequate design can be achieved. It is recommended that the so-called w-plane design method be used, and that the time elapsed before output of the up-dated coil-force signal be kept as small as possible. However, the cycle time for the controller should be watched carefully, because very small values for this time can lead to digital noise.
Document ID
19870018271
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Haviland, J. K.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:181253
UVA/528224-MAE86-105
NASA-CR-181253
Report Number: NAS 1.26:181253
Report Number: UVA/528224-MAE86-105
Report Number: NASA-CR-181253
Accession Number
87N27704
Funding Number(s)
CONTRACT_GRANT: NAG1-349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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