Abstract
In this article, an intelligent predictor-corrector entry guidance approach for lifting hypersonic vehicles is proposed to achieve real-time and safe control of entry flights by leveraging the deep neural network (DNN) and constraint management techniques. First, the entry trajectory planning problem is formulated as a univariate root-finding problem based on a compound bank angle corridor, and two constraint management algorithms are presented to enforce the satisfaction of both path and terminal constraints. Second, a DNN is developed to learn the mapping relationship between the flight states and ranges, and experiments are conducted to verify its high approximation accuracy. Based on the DNN-based range predictor, an intelligent, multiconstrained predictor-corrector guidance algorithm is developed to achieve real-time trajectory correction and lateral heading control with a determined number of bank reversals. Simulations are conducted through comparing with the state-of-the-art predictor-corrector algorithms, and the results demonstrate that the proposed DNN-based entry guidance can achieve the trajectory correction with an update frequency of 20 Hz and is capable of providing high-precision, safe, and robust entry guidance for hypersonic vehicles.
| Original language | English |
|---|---|
| Article number | 9163239 |
| Pages (from-to) | 325-340 |
| Number of pages | 16 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 57 |
| Issue number | 1 |
| DOIs | |
| State | Published - Feb 2021 |
| Externally published | Yes |
Keywords
- Constraint management
- deep neural networks (DNNs)
- entry guidance
- lateral heading control
- numerical predictor-corrector guidance (NPCG)
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