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Title: Rocket tracking and decoupling eigenstructure control law
Keywords: Attitude Control
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.
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Appears in Collections:Technology and Engineering

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