PWM Modeling for Attitude Control of a Launcher During Ballistic Phase and Comparative Stability Analysis
| Autor: | Carsten W. Scherer, Julien Chaudenson, Dominique Beauvois, C. Frechin, Samir Bennani, Martine Ganet-Schoeller, Guillaume Sandou |
|---|---|
| Přispěvatelé: | Supélec Sciences des Systèmes (E3S), Ecole Supérieure d'Electricité - SUPELEC (FRANCE), Astrium Space Transportation (AST), ASTRIUM, University of Stuttgart |
| Jazyk: | angličtina |
| Rok vydání: | 2012 |
| Předmět: |
0209 industrial biotechnology
Engineering business.industry 020208 electrical & electronic engineering Phase (waves) Angular velocity 02 engineering and technology 7. Clean energy Stability (probability) Computer Science::Other [SPI.AUTO]Engineering Sciences [physics]/Automatic Attitude control Double integrator 020901 industrial engineering & automation Control theory Computer Science::Systems and Control 0202 electrical engineering electronic engineering information engineering business Space vehicle Actuator Pulse-width modulation |
| Zdroj: | ROCOND'12 ROCOND'12, Jun 2012, Aalborg, Denmark. pp.CD-Rom, ⟨10.3182/20120620-3-DK-2025.00109⟩ ROCOND |
| DOI: | 10.3182/20120620-3-DK-2025.00109⟩ |
| Popis: | International audience; The present paper exposes a novel description of the effect of a pulse generator on a double integrator representing one axis of rotation for a space vehicle. By considering the difference between the angular velocity obtained with zero-order-hold (ZOH) actuator and the one with a PWM actuator, a perturbation operator expressing the influence of the PWM on the angular speed is defined. Using this configuration in a linear fractional representation (LFR), a stability analysis allows comparing LMI-based and IQC-based stability results for a one degree of freedom rotating body with uncertain PWM and saturation and permits dwelling on improvements to make for further analyses. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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