Gas generator pressure control in throttleable ducted rockets: A classical and adaptive control approach
Author
Alan, A.
Yildiz, Y.
Poyraz, U.
Olgun, U.
Date
2015Source Title
51st AIAA/SAE/ASEE Joint Propulsion Conference
Publisher
American Institute of Aeronautics and Astronautics Inc, AIAA
Language
English
Type
Conference PaperItem Usage Stats
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Metadata
Show full item recordAbstract
This paper describes the control of gas generator pressure in throttleable ducted rockets using nonlinear adaptive control as well as classical control approaches. Simulation results using the full nonlinear and time-varying dynamics of the gas generator are reported in both classical controller and adaptive controller cases. "Closed-loop Reference Model" structure is used together with the adaptive controller to improve transient response. Controllers are simulated to test their robustness by introducing uncertinities, disturbances and noise to the system. Cold Air Test Plant (CATP) is used as the test facility to compare the controllers and validate the results from simulations. Moreover, damping effect of CRM to oscillations in adaptive controller case is observed in CATP tests. © 2015 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Keywords
Adaptive controlClassical control
Closed-loop reference model
Cold air test plant
Pressure control
Throttleable ducted rockets
Adaptive control systems
Controllers
Gas generators
Pressure control
Propulsion
Rockets
Testing
Adaptive Control
Classical control
Ducted rocket
Reference modeling
Test plants
Model reference adaptive control
Permalink
http://hdl.handle.net/11693/28030Collections
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