1990 American Control Conference 1990
DOI: 10.23919/acc.1990.4791146
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Time-Optimal Aircraft Pursuit-Evasion with A Weapon Envelope Constraint

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Cited by 6 publications
(2 citation statements)
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“…The values of first order differential of V , γ and Ψ are denoted as V & , γ& and ψ& respectively, as shown in (4), (5) and (6), where x n , z n and φ are three control variables of CGF.…”
Section: Intelligent Automatic Manoeuvring Mechanism For Computer Genmentioning
confidence: 99%
“…The values of first order differential of V , γ and Ψ are denoted as V & , γ& and ψ& respectively, as shown in (4), (5) and (6), where x n , z n and φ are three control variables of CGF.…”
Section: Intelligent Automatic Manoeuvring Mechanism For Computer Genmentioning
confidence: 99%
“…The theory provides optimal strategies for both pursuer and evader in air combat scenarios. The references [4,5,6] used differential game to obtain best maneuvers for pursuer and evader in special occasions of air combat.…”
mentioning
confidence: 99%