Adaptive energy management for vertical speed control of an airc

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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244178, 244187, G05D 108

Patent

active

040320936

ABSTRACT:
A system for generating an optimum vertical speed command and controlling the aircraft to this command by allowing the aircraft to assume an optimum trimmed condition for the thrust energy available which system utilizes the aircraft autopilot system.

REFERENCES:
patent: 3333795 (1967-08-01), Hattendorf et al.
patent: 3578268 (1971-05-01), Kramer
patent: 3578269 (1971-05-01), Kramer et al.
patent: 3618878 (1971-11-01), Klein
patent: 3801049 (1974-04-01), Simpson et al.

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