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http://dspace.mediu.edu.my:8181/xmlui/handle/123456789/4591| Title: | Rocket tracking and decoupling eigenstructure control law |
| Keywords: | Attitude Control Decoupling Eigenstructure Assignment |
| Issue Date: | 30-May-2013 |
| Publisher: | The Brazilian Society of Mechanical Sciences |
| 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. |
| URI: | http://koha.mediu.edu.my:8181/jspui/handle/123456789/4591 |
| Other Identifiers: | http://www.scielo.br/scielo.php?script=sci_arttext&pid=S0100-73862000000200002 http://www.doaj.org/doaj?func=openurl&genre=article&issn=01007386&date=2000&volume=22&issue=2&spage=149 |
| Appears in Collections: | Technology and Engineering |
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