Lateral pulse jet control of a direct fire atmospheric rocket using an inertial measurement unit sensor system
Impact point dispersion of a direct fire rocket can be drastically reduced with a ring of appropriately sized lateral pulse jets coupled to a trajectory tracking flight control system. The system is shown to work well against uncertainty in the form of initial off-axis angular velocity perturbations...
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| Language: | en_US |
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2012
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| Online Access: | http://hdl.handle.net/1957/32379 |