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A complete flight control scheme with detailed design methodology is proposed for an indoor miniature coaxial helicopter with fixed collective pitch. To avoid system complexity and the problem of minimum phase control, the helicopter dynamic model is decomposed into two cascaded subsystems: an inner one for attitude and heading control and the outer one for trajectory control. H-infinity control technique...
This paper discusses the development of guidance scheme for multiple missiles co-operation engagement. Firstly, based on the intercept point, the mid-course guidance out of the aerosphere is studied to obtain the shutdown condition. Secondly, using the the linearization of the control model and error feedback loop in the mid-course guidance out of the aerosphere, a new guidance law called ITCG (Impact-Time-Control...
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