Abstract
Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance (IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-maker should be limited to a range as small as possible. This paper presents a numerical method for computing the maximal admissible mode decision delay that varies with time-to-go. Particular attention has been paid to highly maneuvering target interception in terminal guidance. The results of this research offer useful guidelines for the design of the mode decision-maker in IEG systems.
| Original language | English |
|---|---|
| Pages (from-to) | 1959-1966 |
| Number of pages | 8 |
| Journal | Chinese Journal of Aeronautics |
| Volume | 32 |
| Issue number | 8 |
| DOIs | |
| State | Published - Aug 2019 |
| Externally published | Yes |
Keywords
- Highly maneuvering target interception
- Integrated Estimation and Guidance
- Maximal admissible mode decision delay
- Mode decision-maker
- Numerical methods