Abstract
The guidance algorithm is the central decision and control element of a missile system. It is responsible for taking data from all available missile sensors, together with targeting information and generating a guidance demand. This is usually in the form of an acceleration demand that is passed to the autopilot.
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© 2001 Springer Science+Business Media New York
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Salmond, D., Gordon, N. (2001). Particles and Mixtures for Tracking and Guidance. In: Doucet, A., de Freitas, N., Gordon, N. (eds) Sequential Monte Carlo Methods in Practice. Statistics for Engineering and Information Science. Springer, New York, NY. https://doi.org/10.1007/978-1-4757-3437-9_25
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DOI: https://doi.org/10.1007/978-1-4757-3437-9_25
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