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Synthesis of full authority flight vehicle autopilots using feedback linearisation has been previously discussed in the literature. The main concern expressed regarding the use of feedback linearization theory for flight control system design has been the issue of the controller stability and performance under modeling inaccuracies and disturbances. This paper advances a method based on differential...
Optimal pursuit-evasion problem between two aircraft including nonlinear point-mass vehicle models and a realistic weapon envelope is analyzed. Using a linear combination of flight time and the square of the vehicle acceleration as the performance index, closed form solution is obtained in nonlinear feedback form. Due to its modest computational requirements, this guidance law useful for on-board...
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