Differential Game Guidance Versus Proportional Navigation for an Air-to- Air Missile

reportActive / Technical Report | Accession Number: ADA019326 | Open PDF

Abstract:

Proportional navigation is a closed loop optimal control for the case of a linear dynamic model of the air-to-air missile intercept problem and a quadratic cost function. This paper presents a differential game model of the intercept problem using nonlinear realistic dynamics, free final time and a terminal cost function related to probability of kill. With this model proportional navigation is no longer optimal and the extent of its nonoptimality is indicated for a range of saddle point solutions. A guidance concept based on differential game theory is discussed and is compared to proportional navigation in an off lime simulation. The considerable gains made by this scheme over proportional navigation provide the incentive to develop a real time version.

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Subject Terms