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This paper describes the continuing project adaptive nonlinear dynamic inversion (ANDI). The ANDI autopilot uses nonlinear dynamic inversion with an adaptive element to account for any errors in the inversion. A reference model is included to provide the desired output performance. This allows the missile performance to be tuned by simply adjusting the(More)
Traditional missile autopilot design typically uses a three loop feedback topology with gains dependent on the current flight condition of the missile. These gain values are obtained by interpolation on a predefined gain table. The gain values that make up this table are designed to balance performance and stability on the grid of flight conditions that(More)
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