SBIR-STTR Award

Scanning Laser Aircraft Surveillance System for Carrier Flight Operations
Award last edited on: 9/5/2002

Sponsored Program
SBIR
Awarding Agency
DOD : Navy
Total Award Amount
$738,000
Award Phase
2
Solicitation Topic Code
N87-208
Principal Investigator
Alan A Vetter

Company Information

Humbug Mountain Research Laboratories

PO Box 1380
Duarte, CA 91009
   (626) 303-2400
   alanvetter@aol.com
   N/A
Location: Single
Congr. District: 32
County: Los Angeles

Phase I

Contract Number: N68335-90-C-0350
Start Date: 00/00/00    Completed: 00/00/00
Phase I year
1990
Phase I Amount
$50,000
The scanning laser aircraft surveillance system (SLASS) uses two scanning laser beams to illuminate approach corridors and retro reflectors located on aircraft landing gears to determine very precisely the azimuthal, ascension, yaw, roll, and pitch angles of carrier approaching aircraft. The range, approach velocity, and aircraft type are also determined. The position of the aircraft is determined by the time for the scanning beam to travel between retroreflectors; optical resolution of the aircraft is not required. Since the laser beams are infrared, low power, and highly directional, they have a very low probability of spurious intercept. The feasibility of the SLASS, together with complementary sensors, to perform aircraft surveillance, aircraft tracking, aircraft configuration, and automatic aircraft type identification will be evaluated with a systems approach. This effort also includes trade-off studies and quantitative analysis of candidate SLASS configurations and options. The goal of this effort is to provide improved information on the approaching aircraft to the LSO and CATC to reduce landing mishaps and missed landings.

Phase II

Contract Number: N68335-90-C-0350
Start Date: 9/11/1990    Completed: 1/10/1992
Phase II year
1990
Phase II Amount
$688,000
The Scanning Laser Aircraft Surveillance System (SLASS) uses two scanning laser beams to illuminate approach corridors with retroreflectors located on aircraft landing gears and hook to determine very precisely the azimuthal, ascension, yaw, roll, and pitch angles of carrier approaching aircraft. The range, approach velocity, and aircraft type are also determined. Aircraft configuration is determined by the presence or absence in one of the retroreflectors. The position of the aircraft is determined by the time for the beams to scan between retroreflectors. Since the laser beams are infrared, low power, and highly directional, they have a very low probability of spurious intercept. A full scale SLASS test unit will be built. The ability of the SLASS to perform aircraft surveillance, aircraft tracking, aircraft configuration, and automatic aircraft type identification will be proven with the test unit. The goal of this effort is to provide improved information on the approaching aircraft to the LSO and CATCC to reduce landing mishaps and missed landings.