Adaptive Pressure Control for Use in Variable-Thrust Rocket Development
For rocket propulsion engineers, this work provides a practical adaptive control solution for throttleable rocket gas generators, though it is an incremental improvement over existing adaptive methods.
The paper proposes a delay-resistant adaptive controller for gas generator pressure control in variable-thrust ducted rockets, achieving improved transient response and effective handling of time delays and uncertainties, validated through simulation and experimental comparisons.
The precise control of gas generator pressure is important to obtain variable thrust in ducted rockets. A delay resistant closed loop reference model adaptive control is proposed in this paper to address this problem. The proposed controller combines delay compensation and adaptation with improved transient response. The controller is successfully implemented using an industrial grade cold air test setup, which is a milestone towards obtaining a fully developed throttleable rocket gas generator controller. Simulation and experimental comparisons with alternative adaptive approaches and a fixed controller demonstrate improved performance and effective handling of time delays and uncertainties. A step by step design methodology, covering robustfying schemes, selection of adaptation rates and initial controller parameters, is also provided to facilitate implementations.