A Guidance Method for Impact Time and Angle Control Based on Trajectory Tracking

Gang Lei, He Wang, Shaopeng Li

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DOI: 10.1155/ijae/5533692
Published: 2025-01
Container: International Journal of Aerospace Engineering
Publisher: Wiley
Open access: unknown

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Cite this work

BibTeX

@article{allodium:10.1155/ijae/5533692,
  title = {A Guidance Method for Impact Time and Angle Control Based on Trajectory Tracking},
  author = {Gang Lei and He Wang and Shaopeng Li},
  year = {2025},
  journal = {International Journal of Aerospace Engineering},
  doi = {10.1155/ijae/5533692},
  url = {https://doi.org/10.1155/ijae/5533692}
}

RIS

TY  - JOUR
TI  - A Guidance Method for Impact Time and Angle Control Based on Trajectory Tracking
AU  - Gang Lei
AU  - He Wang
AU  - Shaopeng Li
PY  - 2025
JO  - International Journal of Aerospace Engineering
DO  - 10.1155/ijae/5533692
UR  - https://doi.org/10.1155/ijae/5533692
ER  -

APA

Lei, G., Wang, H., & Li, S. (2025). A Guidance Method for Impact Time and Angle Control Based on Trajectory Tracking. International Journal of Aerospace Engineering. https://doi.org/10.1155/ijae/5533692

Source records

crossref · retrieved 2026-09-25T15:41:47.267Z