Abstract
Range is one of the main performances of air-to-air missiles (AAMs) to pursue, and one of the key measures is to optimize AAMs’ guidance algorithm. An advanced engineering guidance scheme is proposed based on the idea of piecewise trajectory-shaping, and the optimization of design parameters is completed based on the standard particle swarm optimization algorithm (SPSO). Simulation and optimization results draw some beneficial conclusions, providing new ideas for AAMs’ advanced navigation and guidance modes. Polynomial fitting or looking-up table and interpolation can be applied to realize the optimal guidance scheme in engineering. Simulations show that the trajectory obtained from polynomial fitting parameters is very close to that based on SPSO, which provides an effective way for applications in engineering.
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Li, X., Fu, S., Fan, H. (2013). Optimization of an Advanced Guidance Scheme for Long-Range AAMs Based on SPSO. In: Sun, Z., Deng, Z. (eds) Proceedings of 2013 Chinese Intelligent Automation Conference. Lecture Notes in Electrical Engineering, vol 254. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38524-7_38
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DOI: https://doi.org/10.1007/978-3-642-38524-7_38
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