초록 ▼

A method and system to rapidly, passively, range and track maneuvering airborne emitters (enemy targets and threats) for tactical fighters using batch based recursive estimators for track initialization and track maintenance that includes providing information processing that has angle and signal am

A method and system to rapidly, passively, range and track maneuvering airborne emitters (enemy targets and threats) for tactical fighters using batch based recursive estimators for track initialization and track maintenance that includes providing information processing that has angle and signal amplitude data, threat database, and feedback from pilot cue analysis. The system includes pilot cue analysis which computes airborne emitter (target and threat) heading and corresponding accuracy to determine if sufficient accuracy is available to present the pilot with proper pilot cue options. The first stage is a range bank also called a compound parallel hypothesis evaluator and the second stage is an interactive multi-model. Both stages provide for the output of the algorithm to be a range measurement and an associated confidence factor. The algorithm inputs azimuth angle elevation angle and range and is capable of inputting data from three different data pre-processors (i.e., sensor data fusion).

대표청구항 ▼

What is claimed is: 1. A method to rapidly, passively range and track maneuvering airborne emitters for tactical fighters that includes batch based maximum likelihood probabilistic data association for track initialization and interacting multiple model estimators for track maintenance, comprising

What is claimed is: 1. A method to rapidly, passively range and track maneuvering airborne emitters for tactical fighters that includes batch based maximum likelihood probabilistic data association for track initialization and interacting multiple model estimators for track maintenance, comprising the steps of: providing track initialization by providing and including an ML-PDAF filter; providing track maintenance using interacting multiple model PDAF with amplitude information; providing information processing connected to the input of said track initialization filter, which includes threat database information, angle and signal amplitude data, and ownship inertial data; providing pilot cue analysis to the pilot of said tactical fighter that includes pilot cues for turning for more rapid problem solving; providing emitter airborne track information; and maintaining track whenever the airborne emitter target or threat maneuvers using angle measurements. 2. A method to rapidly, passably range and track maneuvering airborne emitters (targets) for tactical fighters to meet passive geolocation quality performance against an active airborne emitter (target) using only the tactic fighter passive RF multifunction aperture (MFA) azimuth measurements along with prescribed tactical fighter maneuvers wherein geolocation involves estimating target state vector and error covariance including range, speed, heading, azimuth and elevation comprising the steps of: providing track initialization by providing and including an ML-PDAF filter; providing track maintenance using interacting multiple model PDAF with amplitude information; providing information processing connected to the input of said track. initialization filter, which includes threat database information, angle and signal amplitude data, and ownship inertial data; providing pilot cue analysis to the pilot of said tactical fighter that includes pilot cues for turning for more rapid problem solving; providing emitter airborne track information; maintaining track whenever the airborne emitter target or threat maneuvers using angle measurements; providing a Kalman filter-based algorithm that includes a first stage and a second stage; providing in said first stage of said Kalman filter-based algorithm for monitoring the measurement residuals by processing measured MFA azimuth data over a set of candidate initial state vectors to weed out improbable geolocation solutions and converge to the most likely to effectively initialize the Kalman filter state vector; and providing a second stage that continues processing subsequent angled measurements in the two model interacting multiple models whereby the airborne target dynamics are modeled as (1) straight which include constant speed and heading; and (2) undergoing a maneuver including a heading change over a brief period of time.