@inproceedings{8666b98715a4478fb41fb504a1e4cb1c,
title = "Rapid prototyping of a guidance and control system for missiles",
abstract = "This paper describes rapid prototyping of a guidance and control system for missiles to improve its overall design process effectiveness. A rapid prototyping design process is developed based on MATLAB/Simulink/RTW and Skyfly. An air-to-surface missile is used as a design example. A high fidelity 6-DOF missile simulation model is built for rapid prototyping test and a trimmed simulation model is presented as validation and linear equations of motion are provided for guidance and control analysis. Simulation study results indicate that the proposed rapid prototyping process is practically feasible for effectively developing a guidance and control system of an air-to-surface missile.",
author = "Binfeng Pan and Shuo Tang and Bong Wie",
year = "2008",
doi = "10.2514/6.2008-7003",
language = "英语",
isbn = "9781563479458",
series = "AIAA Guidance, Navigation and Control Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "AIAA Guidance, Navigation and Control Conference and Exhibit",
}