Walking the Precession for Trajectory Control of Munitions

No AccessWalking the Precession for Trajectory Control of MunitionsBoris Kogan and Ephrahim GarciaBoris KoganCornell University, Ithaca, New York 14853*Graduate Research Assistant, Sibley School of Mechanical and Aerospace Engineering, 138 Upson Hall.Search for more papers by this author and Ephrahim GarciaCornell University, Ithaca, New York 14853†Professor, Sibley School of Mechanical and Aerospace Engineering, 224 Upson Hall. Associate Fellow AIAA.Search for more papers by this authorPublished Online:29 Apr 2014https://doi.org/10.2514/1.G000258SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Barrett R. and Lee G., “Design and Testing of Piezoelectric Flight Control Actuators for Hard-Launch Munitions,” SPIE 11th Annual International Symposium on Smart Structures and Materials, International Society for Optics and Photonics, San Diego, CA, March 2004, pp. 459–470. Google Scholar[2] Fresconi F. and Plostins P., “Control Mechanism Strategies for Spin-Stabilized Projectiles,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 224, No. 9, 2010, pp. 979–991. doi:https://doi.org/10.1243/09544100JAERO705 CrossrefGoogle Scholar[3] Ollerenshaw D. and Costello M., “Simplified Projectile Swerve Solution for General Control Inputs,” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 5, 2008, pp. 1259–1265. doi:https://doi.org/10.2514/1.34252 JGCDDT 0162-3192 LinkGoogle Scholar[4] Cooper G. and Costello M., “Flight Dynamic Response of Spinning Projectiles to Lateral Impulsive Loads,” Journal of Dynamic Systems, Measurement, and Control, Vol. 126, No. 3, 2004, pp. 605–613. doi:https://doi.org/10.1115/1.1789976 JDSMAA 0022-0434 CrossrefGoogle Scholar[5] Salman M. U. and Chang B., “Active Coning Compensation for Control of Spinning Flying Vehicles,” Proceedings of the 2010 IEEE International Conference on Control Applications, 2010, pp. 1832–1837. Google Scholar[6] Corriveau D., Wey P. and Berner C., “Thrusters Pairing Guidelines for Trajectory Corrections of Projectiles,” Journal of Guidance, Control, and Dynamics, Vol. 34, No. 4, 2011, pp. 1120–1128. doi:https://doi.org/10.2514/1.51811 JGCDDT 0162-3192 LinkGoogle Scholar[7] McCoy R., Modern Exterior Ballistics: The Launch and Flight Dynamics of Symmetric Projectiles, Schiffer, Atglen, PA, 2012. Google Scholar[8] McCoy R., The Aerodynamic Characteristics of .50 Ball, M33, Api, M8, and Apit, M20 Ammunition, Defense Technical Information Center, Ft. Belvoir, VA, 1990. Google Scholar[9] Dykes J., Montalvo C., Costello M. and Sahu J., “Use of Microspoilers for Control of Finned Projectiles,” Journal of Spacecraft and Rockets, Vol. 49, No. 6, 2012, pp. 1131–1140. doi:https://doi.org/10.2514/1.A32274 JSCRAG 0022-4650 LinkGoogle Scholar[10] Burcheff B. and Costello M., “Model Predictive Lateral Pulse Jet Control of an Atmospheric Rocket,” Journal of Guidance, Control, and Dynamics, Vol. 25, No. 5, 2002, pp. 860–867. doi:https://doi.org/10.2514/2.4979 JGCDDT 0162-3192 LinkGoogle Scholar[11] Gross S., Costello M. and Fresconi F., “Impact Point Model Predictive Control of a Spin-Stabilized Projectile with Instability Protection,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2013 (in press). doi:https://doi.org/10.1177/0954410013514743 Google Scholar[12] Ollerenshaw D. and Costello M., “Model Predictive Control of a Direct Fire Projectile Equipped with Canards,” Journal of Dynamic Systems, Measurement, and Control, Vol. 130, No. 6, 2008, Paper 061010. doi:https://doi.org/10.1115/1.2957624 JDSMAA 0022-0434 CrossrefGoogle Scholar Previous article Next article