ADAPTIVE NOISE CANCELLATION IN A CLOSED LOOP CONTROL SYSTEM
Assignee
HUGHES AIRCRAFT COMPANY, LOS ANGELES, CALIFORNIA, A DE CORP.
Filed
Jul 17, 1987
Granted
Oct 20, 1992
Location
Albuquerque NM (Kirtland AFB/Sandia)
Abstract
An adaptive noise cancellation system reduces undesired noise in a closed loop control system by injecting an adaptively constructed noise cancellation signal at an appropriate point in the closed control loop. The generation of a compensation filter N for adaptive noise cancellation loop error signal is disclosed by two methods. A first method is an inverse error rejection response (IERR) method. A second method optimally matches spectrums of a noise signal and a noise reference signal at the adaptive noise cancellation system. This second method is referred to as a spectral matching (SM) method.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 12, 1989
Rescinded
Apr 2, 1992
Duration
2 years, 11 months
Inventor
- 1JERRY M. ALCONE
Sensitive facility: Albuquerque NM (Kirtland AFB/Sandia)
Record Details
- Patent number
- US 5157596
- Application
- 07075013
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records