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- W2325335710 abstract "Isaac Kaminer Patrick O'Shaughnessy The Boeing Company Seattle, Washington 98124-2207 Presented here is a design of the four-dimensional (4D) mode for an integrated autopilot/autothrottle control system named TECS. This design involves integrating a 4D flight trajectory generator with TECS, creating an outer loop time error control law, and integrating spoilers with TECS to increase the energy bleed-off capacity of the system during descent. The resulting system follows a precomputed 4D profile in cruise, except if there is a large time error when the system is engaged. In such a case, the system generates a speed profile to null out the time error by the top of descent. During descent, the system follows a fixed profile by employing both throttles and spoilers." @default.
- W2325335710 created "2016-06-24" @default.
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- W2325335710 date "1988-08-15" @default.
- W2325335710 modified "2023-10-18" @default.
- W2325335710 title "4D-TECS integration for NASA TCV airplane" @default.
- W2325335710 cites W2332249232 @default.
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- W2325335710 doi "https://doi.org/10.2514/6.1988-4067" @default.
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