Evaluation of a multivariable control design on a variable cycle engine simulation-Reference-Cited by-同舟云学术

Evaluation of a multivariable control design on a variable cycle engine simulation

Published:1982-06-21 Issue: Volume: Page:
ISSN:
Container-title:18th Joint Propulsion Conference
language:
Short-container-title:

Author:

PRZYBYLKO S.¹,ROCK S.²

Affiliation:

1. USAF, Aero Propulsion Laboratory, Wright-PattersonAFB, OH

2. Systems Control Technology, Inc., Palo Alto, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1077

Reference31 articles.

1. Failure accomnodation i s provided throughout the logic. Thrust, airflow, and mode inputs are monitored according t o slew rate and a11owable range. Sensor inputs have f u l l analytical redundancy i n the fault-tolerant filter. Control commands are monitored for abnormal conditions and servo error signal response i s monitored t o detect failed output servos. Computer Simulation and Evaluation Procedure

2. PLA * 30-32-30

3. PLA = 49-50-49 discussed. The engine designer observed that the trajectory generator and respective controller outputs occasionally moved i n a direction opposite to the commanded change i n steady-state

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