No AccessEstimation Enhancement by Imposing a Relative Intercept Angle for Defending MissilesRobert Fonod and Tal Y. ShimaRobert FonodTechnion--Israel Institute of TechnologySearch for more papers by this author and Tal Y. ShimaTechnion--Israel Institute of TechnologySearch for more papers by this authorAIAA 2017-1018Session: Missile Intercept and Evasion GuidancePublished Online:5 Jan 2017https://doi.org/10.2514/6.2017-1018SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byA Convex Programming-Based Approach to Trajectory Optimization for Survivability Enhancement of Homing Missiles18 August 2022 | International Journal of Aeronautical and Space Sciences, Vol. 23, No. 5Optimal Cooperative Guidance Strategies for Aircraft Defense with Impact Angle Constraints12 November 2022 | Aerospace, Vol. 9, No. 11Weapon–Target-Allocation Strategies in Multiagent Target–Missile–Defender EngagementVitaly Shalumov and Tal Shima26 June 2017 | Journal of Guidance, Control, and Dynamics, Vol. 40, No. 10Estimation Enhancement by Cooperatively Imposing Relative Intercept AnglesRobert Fonod and Tal Shima3 April 2017 | Journal of Guidance, Control, and Dynamics, Vol. 40, No. 7 What's Popular AIAA Guidance, Navigation, and Control Conference 9 - 13 January 2017Grapevine, Texashttps://doi.org/10.2514/6.2017-1018 CrossmarkInformationCopyright © 2017 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAeronauticsAir NavigationAircraft Navigation SystemsAvionicsControl TheoryGuidance and Navigational AlgorithmsGuidance, Navigation, and Control SystemsGuided MissilesMilitary ScienceMilitary TechnologyMissile Guidance and ControlMissile Systems, Dynamics and TechnologyMissilesSensorsTransducersWeapon Systems KeywordsHoming MissileGuidance SystemFlight Path AngleIntercept Angle Guidance LawTarget MissilesCumulative Distribution FunctionInertial Navigation SystemNumerical IntegrationEngagement KinematicsMissile DynamicsDigital Topics Guidance, Navigation, and Control