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DC Field | Value | Language |
---|---|---|
dc.creator | Oliva P. | - |
dc.creator | Leite Filho W. C. | - |
dc.date | 2000 | - |
dc.date.accessioned | 2013-05-30T11:25:51Z | - |
dc.date.available | 2013-05-30T11:25:51Z | - |
dc.date.issued | 2013-05-30 | - |
dc.identifier | http://www.scielo.br/scielo.php?script=sci_arttext&pid=S0100-73862000000200002 | - |
dc.identifier | http://www.doaj.org/doaj?func=openurl&genre=article&issn=01007386&date=2000&volume=22&issue=2&spage=149 | - |
dc.identifier.uri | http://koha.mediu.edu.my:8181/jspui/handle/123456789/4591 | - |
dc.description | A control law was designed for a satellite launcher ( rocket ) vehicle using eigenstructure assignment in order that the vehicle tracks a reference attitude and also to decouple the yaw response from roll and pitch manoeuvres and to decouple the pitch response from roll and yaw manoeuvres. The design was based on a complete linear coupled model obtained from the complete vehicle non linear model by linearization at each trajectory point. After all, the design was assessed with the vehicle time varying non-linear model showing a good performance and robustness. The used design method is explained and a case study for the Brazilian satellite launcher ( VLS Rocket ) is reported. | - |
dc.publisher | The Brazilian Society of Mechanical Sciences | - |
dc.source | Journal of the Brazilian Society of Mechanical Sciences | - |
dc.subject | Attitude Control | - |
dc.subject | Decoupling | - |
dc.subject | Eigenstructure Assignment | - |
dc.title | Rocket tracking and decoupling eigenstructure control law | - |
Appears in Collections: | Technology and Engineering |
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