A Robust Predefined Performance Controller for Reusable Launch Vehicles Under Mismatched Disturbance and Input Saturation
Source abstract
Abstract
This paper addresses the attitude tracking control issue for reusable launch vehicles (RLVs) in the presence of non-matching disturbances and saturation effects. An enhanced predefined performance function (PPF) is derived based on a novel anti-saturation predefined-time compensator (ASPC) to ensure stability during saturation. Additionally, a fixed-time disturb observer (DO) is introduced for estimating both mismatch and matching perturbations within a fixed-time interval. Based on the error transformation, a fixed-time dynamic surface control (DSC) is proposed, ensuring that the transformed system state converges to the residual set at the origin promptly. The simulations demonstrate that the attitude tracking error reliably converges to a predefined region within a predetermined time.
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Research context
OpenAlex topics: Adaptive Control of Nonlinear Systems · Spacecraft Dynamics and Control · Inertial Sensor and Navigation
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
Beijing Institute of Electronic System Engineering, Beijing 100854, China
Shenyang Aircraft Design and Research Institute, Aviation Industry Corporation of China, Ltd., Shenyang 110035, China
Funding
the National Natural Science Foundation of China
References (31)
Show source-provided references
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