Integrated fire and flight control system for controlling the an

Details Integrated fire and flight control system for controlling the an Integrated fire and flight control system for controlling the an

1998-03-31

2000-11-14

Johnson, Stephen M.

Ordnance

Mounts

Training mechanisms

244 1713, F41G 322

Patent

active

061454281

ABSTRACT:
An integrated fire and flight control system of the type which controls aircraft flight dynamics to referenced values defined by a weapon launch solution to provide optimum aircraft to target orientation, further optimizes the aircraft's angle of attack (AOA) to the target by controlling the aircraft's vertical speed to modify the aircraft's rate of climb or descent as necessary to produce an actual pitch attitude that is within a range of AOA values corresponding to the range of permissive weapon launch vertical speeds recommended by the weapons manufacturer.

REFERENCES:
patent: 5195700 (1993-03-01), Fogler, Jr. et al.
patent: 5222691 (1993-06-01), Gold et al.
patent: 5238203 (1993-08-01), Skonieczy et al.
patent: 5263662 (1993-11-01), Fowler et al.
patent: 5310135 (1994-05-01), Fowler et al.
patent: 5310136 (1994-05-01), Fowler et al.
patent: 5331881 (1994-07-01), Fowler et al.
patent: 5428543 (1995-06-01), Gold et al.
patent: 5465212 (1995-11-01), Fowler et al.
System Development Report, May 1996 (pp. 35-27 only).
Preliminary Design Review, May 1996 (slide PDR-11 only).
System Development Report, Mar. 24, 1997 (see pp. 35-37) pp. 1-71.
Development Review Briefing Notes, Mar. 24, 1997 (see Slides IFFC DR 61-63) DR1-DR80.

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