Design and Analysis of Terminal Guidance Law for Kinetic Interceptors based on Pulse Engine
A new terminal guidance law is proposed based on a solid propellant pulse engine and an improved proportional navigation method to address the terminal guidance issue for kinetic interceptors. On this basis, the start-stop curve of the pulse motor during the terminal guidance process is designed, along with its start-up logic. The effectiveness of the proposed guidance strategy is verified through simulation.
Authors
- Shuai Yue (ORCID: https://orcid.org/0000-0001-6774-7879)
- Shixin Li (ORCID: https://orcid.org/0009-0009-0273-0406)
- Jia Ma
Institutions
- China Academy of Space Technology (CN)
- Nanjing University of Science and Technology (CN)
- China National Space Administration (CN)
Publication Details
- Journal
- Journal of Electronic Research and Application
- Published
- 2024-09-30
- DOI
- https://doi.org/10.26689/jera.v8i5.8400
- Primary Topic
- Guidance and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00