Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method

Authors

Bradley Burchett, Rose-Hulman Institute of TechnologyFollow

Document Type

Article

Publication Date

2013

DOI Number / ISBN

10.1016/j.ast.2013.07.010

External Access URL

http://www.sciencedirect.com/science/article/pii/S1270963813001375

Recommended Citation

Burchett, B.T. (2013). Aerodynamic parameter identification for symmetric projectiles: An improved gradient based method. Aerospace Science and Technology, 30(1), 119-127. https://doi.org/10.1016/j.ast.2013.07.010