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Robust extended state observer-based three dimensional integrated guidance and control design for interceptors with
Saeed Khankalantary1, Farid Sheikholeslam1
1Department of Electrical and Computer Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran.
This study introduces a new integrated guidance and control (IGC) scheme for interceptors, enhancing precision by addressing impact angle and actuator limits. The advanced method ensures robust performance against disturbances and uncertainties.
Area of Science:
- Aerospace Engineering
- Control Systems
- Robotics
Background:
- Interceptor guidance and control (IGC) systems face challenges with impact angle constraints and actuator saturation.
- Existing methods struggle with model uncertainties, external disturbances, and the computational complexity of control signal derivatives.
- Skid-to-turn (STT) interceptors require sophisticated control strategies for accurate targeting.
Purpose of the Study:
- To develop a novel three-dimensional integrated guidance and control (IGC) scheme for skid-to-turn interceptors.
- To incorporate impact angle and actuator saturation constraints into the IGC design.
- To enhance robustness against model uncertainties, external disturbances, and target maneuvers.
Main Methods:
- A six-degrees-of-freedom (6-DOF) realistic model of the interceptor was developed.
- The IGC scheme integrates backstepping, command filtering, sliding mode control (SMC), and super-twisting extended state observer (STESO).
- Command filters address the complexity of virtual control signal derivatives and actuator saturation.
- Finite-time STESO combined with SMC ensures robustness against disturbances and target accelerations.
Main Results:
- The proposed IGC scheme effectively handles impact angle and actuator saturation constraints.
- The integrated approach demonstrates strong robustness against lumped disturbances and target accelerations.
- Lyapunov stability theory confirms system stability and uniformly ultimately boundedness of all states.
- Extensive numerical simulations validate the effectiveness of the developed IGC method.
Conclusions:
- The novel IGC scheme provides a robust and effective solution for skid-to-turn interceptors.
- The method successfully manages complex constraints and uncertainties inherent in missile guidance.
- The findings contribute to the advancement of high-performance guidance and control systems for interceptors.
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