Main Article Content
Abstract
Extension of range of artillery rocket using gliding technique is very effective way. Extension in the range is achieved by control surfaces without adding any extra charge. Controls are applied after completion of launch phase and trajectory is controlled by canards or flat tail control fins. Contribution in this work is to find the optimum time to initiate the controls during the flight so as to get maximum range. Analysis has been carried out using six degree of freedom equations of motion.
Keywords
Article Details
References
- Garnell, P., "Guided Weapon Control Systems", 2nd Edition, Pergamon Press, Oxford, England, 1980.
- McCoy, R. L., "Modern Exterior Ballistics", Schiffer Publication, 1999.
- Wenjun, Yi, Bisheng Zhang and Zhongyan Wang., "Analysis of Ballistic Performance of a Glide Extended-Range Projectile", 21st International Symposium on Ballistics, Adelaide, Australia, 2004, pp.
- -465.
- Grignon, C., Zilliani, A., Fleek, V., David, S. and Arriguci, A., "Steering of a Spin Stabilized Gliding
- Projectile: First Approach", 20th International Symposium on Ballistics, Orlando, 2003, pp.90-98.
References
Garnell, P., "Guided Weapon Control Systems", 2nd Edition, Pergamon Press, Oxford, England, 1980.
McCoy, R. L., "Modern Exterior Ballistics", Schiffer Publication, 1999.
Wenjun, Yi, Bisheng Zhang and Zhongyan Wang., "Analysis of Ballistic Performance of a Glide Extended-Range Projectile", 21st International Symposium on Ballistics, Adelaide, Australia, 2004, pp.
-465.
Grignon, C., Zilliani, A., Fleek, V., David, S. and Arriguci, A., "Steering of a Spin Stabilized Gliding
Projectile: First Approach", 20th International Symposium on Ballistics, Orlando, 2003, pp.90-98.