Tuning Techniques Evaluation for Satellite Launch Vehicle Attitude Controllers

Tuning Techniques Evaluation for Satellite Launch Vehicle Attitude Controllers

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This communication presents a comparative analysis of tuning techniques for satellite launch vehicle attitude controllers. The investigated tuning techniques consist in the minimization of specific performance indexes, namely the Integral Absolute Error (IAE) index, the Integral of Time Multiplied A...

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Bibliographic Details
Main Authors: Felipe Oliveira e Silva, Waldemar de Castro Leite Filho, Alexandro Garro Brito, Adolfo Graciano da Silva
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2019-05-01
Series:Journal of Aerospace Technology and Management
Subjects:
Spacecraft launching
Attitude control
Tuning
Linear quadratic Gaussian control
Performance indexes
Optimization
Online Access:https://www.jatm.com.br/jatm/article/view/1004

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