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Adaptive terminal super-twisting prescribed performance controller for near-space vehicle based on data-driven model.

Tianchen Zhang1, Yibo Ding1, Xiaokui Yue1

  • 1School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China; Research & Development Institute of Northwestern Polytechnical University in Shenzhen, Sanhang Science &Technology Buliding, No. 45th, Gaoxin South 9th Road, Nanshan District, Shenzhen 518063, China; National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an 710072, China.

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A novel controller ensures near-space vehicle performance by using a predetermined-time function and LSTM data. This adaptive super-twisting prescribed performance controller (DASTPC) prevents scramjet choking and improves control accuracy.

Keywords:
Adaptive fast terminal super-twisting algorithmLong-short term memoryNear-space vehiclePredetermined-time prescribed performance function

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Area of Science:

  • Aerospace Engineering
  • Control Systems
  • Artificial Intelligence

Background:

  • Near-space vehicles (NSVs) require advanced control for stable flight and efficient scramjet operation.
  • Traditional controllers struggle with model uncertainties and external disturbances, potentially leading to performance degradation and scramjet choking.

Purpose of the Study:

  • To design a data-driven adaptive terminal super-twisting prescribed performance controller (DASTPC) for NSVs.
  • To ensure transient and steady-state performance while preventing scramjet choking.
  • To enhance control robustness against model uncertainties and external disturbances.

Main Methods:

  • Proposed a novel predetermined-time performance function for faster, more accurate error convergence.
  • Developed a non-singular fast terminal sliding surface and an adaptive super-twisting reaching law for improved efficiency and reduced chattering.
  • Utilized a deep recurrent neural network (LSTM) for a data-driven model to handle NSV dynamics and uncertainties.
  • Employed a homogeneous high-order sliding mode observer to compensate for external disturbances.

Main Results:

  • The DASTPC guarantees tracking error convergence within a predetermined time.
  • The adaptive reaching law effectively tunes control gain, mitigating chattering and excessive gains.
  • The LSTM-based data-driven model successfully suppresses model uncertainties.
  • The controller effectively restricts the angle of attack, ensuring scramjet intake conditions.

Conclusions:

  • The DASTPC demonstrates superior performance in simulations compared to traditional methods.
  • The controller achieves prescribed performance bounds under disturbances and parameter perturbations.
  • The proposed approach enhances NSV flight safety and operational efficiency.