Fuzzy Adaptive Zero-Error-Constrained Tracking Control for HFVs in the Presence of Multiple Unknown Control
This study achieves zero-error tracking for hypersonic flight vehicles (HFVs) despite unknown control directions and asymmetric constraints. Novel control strategies ensure stability and convergence for enhanced flight performance.
Area of Science:
- Aerospace Engineering
- Control Systems Theory
Background:
- Hypersonic flight vehicles (HFVs) face complex control challenges including unknown directions and asymmetric state constraints.
- Existing control methods struggle with simultaneous uncertainties and strict operational boundaries.
Purpose of the Study:
- To develop a robust control methodology for achieving zero-error constrained tracking in HFVs.
- To address challenges posed by unknown control directions and asymmetric flight state constraints.
Main Methods:
- Incorporation of novel Nussbaum functions to handle multiple unknown control directions and ensure integral boundedness.
- Utilization of fuzzy-logic systems (FLSs) for approximating model uncertainties.
- Adoption of asymmetric integral barrier Lyapunov functions (IBLFs) to manage asymmetric flight state constraints.
Main Results:
- Demonstrated convergence of velocity and altitude tracking errors to zero.
- Ensured boundedness of Nussbaum integral terms despite potential cancellations.
- Validated effectiveness in guaranteeing convergence, smoothness, and constraint satisfaction through simulations.
Conclusions:
- The proposed control methodology effectively achieves zero-error tracking for HFVs under challenging conditions.
- The integration of novel Nussbaum functions and IBLFs provides a robust solution for complex flight dynamics.
- The approach successfully handles unknown control directions and asymmetric constraints, enhancing HFV control performance.
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