导航

Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (8): 231148.doi: 10.7527/S1000-6893.2024.31148

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles    

Fault diagnosis of thrust offset loss of launch vehicle based on AGABP neural network

Haipeng CHEN1,2(), Wenxing FU3,4,5, Jie YAN3,4,5   

  1. 1.School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China
    2.China Academy of Launch Vehicle Technology,Beijing 100076,China
    3.National Key Laboratory of Unmanned Aerial Vehicle Technology,Xi’an 710072,China
    4.Integrated Research and Development Platform of Unmanned Aerial Vehicle Technology,Xi’an 710072,China
    5.Unmanned System Research Institute,Northwestern Polytechnical University,Xi’an 710072,China
  • Received:2024-09-03 Revised:2024-10-08 Accepted:2024-11-21 Online:2024-12-09 Published:2024-11-29
  • Contact: Haipeng CHEN E-mail:chenhp_hit@163.com
  • Supported by:
    National Natural Science Foundation of China(52232014)

Abstract:

To address the thrust deviation loss fault in the launch vehicle’s power system, an online detection and diagnosis method for thrust faults based on the Adaptive Genetic Algorithm-based Back Propagation (AGABP) neural network is proposed. To achieve low-latency, high-precision online detection and diagnosis of thrust loss faults, this method solely utilizes the rocket motion information measured by onboard sensors. Firstly, a six-degree-of-freedom (6-DOF) modeling is established based on the data and thrust fault types of a certain type of launch vehicle in China. Historical state information sensitive to faults, such as overload and apparent acceleration, was used as inputs for network training. Secondly, the initial weights in the BP neural network are adjusted through the adaptive genetic algorithm to obtain optimized network parameters. Finally, the resulting online diagnostic model for thrust deviation loss faults in launch vehicles is verified through 6-DOF online simulations. Numerical simulation results indicate that compared with the traditional BP network, the AGABP-based method exhibits faster convergence speed with fewer iteration generations. The accuracy of fault location is 96.51%, the fault location delay is between 0.1 s and 2 s, and the difference between the predicted and actual thrust reduction degree is within 20% for 94.19% of the samples.

Key words: launch vehicle, power system fault, fault detection and diagnosis, adaptive genetic algorithm, neural network

CLC Number: