Abstract
This paper considers the problem of emulating an optimal impactangle-control guidance law using a pursuer guided with proportional navigation by using a virtual target approach. Based on the choice of the lead distance to the virtual targets, two algorithms for the virtual target computation are presented. In the first, the lead distance is specified in advance, whereas in the second, it is optimized. The simulation results demonstrate that the proposed solution can achieve an accurate emulation of the reference guidance law.
Original language | English |
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State | Published - 2023 |
Event | 62nd Israel Annual Conference on Aerospace Sciences, IACAS 2023 - Haifa, Israel Duration: 15 Mar 2023 → 16 Mar 2023 |
Conference
Conference | 62nd Israel Annual Conference on Aerospace Sciences, IACAS 2023 |
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Country/Territory | Israel |
City | Haifa |
Period | 15/03/23 → 16/03/23 |
ASJC Scopus subject areas
- Aerospace Engineering