Aircraft roll steering command system

Details Aircraft roll steering command system Aircraft roll steering command system

1981-08-19

1985-08-06

Chin, Gary

Boots, shoes, and leggings

364428, 244183, G05D 112

Patent

active

045339996

ABSTRACT:
Aircraft roll command signals are generated as a function of the Microwave Landing System based azimuth, groundtrack, groundspeed and azimuth rate or range distance input parameters. On initial approach, roll command signals are inhibited until a minimum roll command requirement is met. As the aircraft approaches the centerline of the runway, the system reverts to a linear track control.

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patent: 3355126 (1967-11-01), Oppedahl
patent: 3573827 (1971-04-01), De Botton
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patent: 4354237 (1982-10-01), Lambregts et al.
Madden et al.; "Nonlinear Trajectory-Following & Control Tech. in Terminal Area Using MLS Navigation Sensor"; Navigation: Jnl. of Inst. of Navigation; vol. 20, No. 4, winter 1973-1974; pp. 285-295.
Minnett et al.; "Interscan--A New Microwave Approach and Landing Guidance System for Int'l Civil Aviation"; AEV (Jnl. of Asia Elect. Union), vol. 7; No. 2, 1974, pp. 15-20.

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