Research/Patents/US 5501413
US 5501413

METHOD AND DEVICE FOR RECOGNIZING DECOYS SERVING TO DISGUISE A TARGET WITH THE AID OF AN ACTIVE SEARCH HEAD

Assignee

DAIMLER-BENZ AEROSPACE AG PATENTE

Filed

Jan 16, 1973

Granted

Mar 26, 1996

Location

POSTFACH 801109, 81663 MUNCHEN GERMANY

Abstract

A guided missile is directed toward a ground level or sea level target despite the presence of laterally and vertically offset decoys by causing the missile first to "acquire" one of the target or decoys. The guidance system then directs the missile in the azimuth plane toward the acquired target while it directs the missile along a predetermined path that ends in a low level horizontal flight. A simulator simulates a flight path toward the acquired target in the elevational plane. When the simulated flight path toward the acquired target deviates from the predetermined elevational path by a preset amount, a logic system causes the missile to unlock from the target and acquire a new one. Thus the missile will ultimately only lock onto the sea level or ground level target.

Source: Google Patents

35 USC §181 Secrecy Order

Imposed

Jan 29, 1982

Rescinded

Jan 7, 1992

Duration

9 years, 11 months

Inventor

  • 1FRIDBERT KILGER

Technology Domains

Click a domain to browse all patents in this category.

Back to patent indexSource: USPTO 35 USC §181 secrecy order records