Simulation of a 6DOF Nonlinear Missile
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-38446-2_46
Reference5 articles.
1. Belkacem, B., & Bachir, N. (2019). Dynamic modeling & control of large space structures: Part I (Issue October).
2. Da Silveira, G., & Carrara, V. (2015). A six degrees-of-freedom flight dynamics simulation tool of launch vehicles. Journal of Aerospace Technology and Management, 7(2), 231–239. https://doi.org/10.5028/jatm.v7i2.433
3. De Marco, A., Duke, E. L., & Berndt, J. S. (2007). A general solution to the aircraft trim problem. https://doi.org/10.2514/6.2007-6703
4. Hang, C. C., Astrom, K. J., & Ho, W. K. (1991). Refinements of the Ziegler-Nichols tuning formula. IEE Proceedings D: Control Theory and Applications, 138(2), 111–118. https://doi.org/10.1049/ip-d.1991.0015
5. Kisabo, A. B., Adebimpe, A. F., Okwo, O. C., & Samuel, S. O. (2019). State-space modelling of a rocket for optimal control system design. Journal of Aircraft and Spacecraft Technology, 3(1), 128–137. https://doi.org/10.3844/jastsp.2019.128.137
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