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- W2078902577 abstract "This paper details the design methodology for a missile digital autopilot using a digitization approach, and a discrete domain design approach. These two designs rely heavily on computerized system analysis tools in the frequency and time domains. Further, three complex frequency planes are available to the designer, therefore, relative merits of each will be discussed.This paper will also detail the implementation of the autopilot on the missile microcomputer, a six degree of freedom (6DOF) missile simulation, and a hardware in the loop (HWIL) hybrid computer simulation. The 6DOF permits fine-tuning of design parameters for optimum system performance, whereas the HWIL simulation exercises the real flight hardware.Finally, this paper will also show the final autopilot design verification through comprehensive deterministic and Monte Carlo simulations." @default.
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- W2078902577 date "1979-12-03" @default.
- W2078902577 modified "2023-09-27" @default.
- W2078902577 title "Computer-aided digital autopilot design & analysis: Methodology, implementation and verification" @default.
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- W2078902577 doi "https://doi.org/10.5555/800089.802854" @default.
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