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 |
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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