TY - GEN
T1 - A Direct Multiple Shooting for the Optimal Trajectory of Missile Guidance
AU - Subchan, S.
PY - 2008
Y1 - 2008
N2 - The optimal solutions of air-to-surface missile using a direct multiple shooting are presented. The missile must attack a fixed target by a vertical dive. The missile guidance problem is reinterpreted using optimal control theory resulting in the formulation of minimum integrated altitude problem. The formulation entails nonlinear, 2-dimensional missile flight dynamics, boundary conditions and path constraints. The influence of the boundary conditions on the structure of the optimal solution and the performance index are investigated. The results are then interpreted from the operational and computational perspective.
AB - The optimal solutions of air-to-surface missile using a direct multiple shooting are presented. The missile must attack a fixed target by a vertical dive. The missile guidance problem is reinterpreted using optimal control theory resulting in the formulation of minimum integrated altitude problem. The formulation entails nonlinear, 2-dimensional missile flight dynamics, boundary conditions and path constraints. The influence of the boundary conditions on the structure of the optimal solution and the performance index are investigated. The results are then interpreted from the operational and computational perspective.
KW - Direct multiple shooting
KW - Missile guidance
KW - Optimal control
UR - http://www.scopus.com/inward/record.url?scp=53349175460&partnerID=8YFLogxK
U2 - 10.1109/CCA.2008.4629675
DO - 10.1109/CCA.2008.4629675
M3 - Conference contribution
AN - SCOPUS:53349175460
SN - 9781424422234
T3 - Proceedings of the IEEE International Conference on Control Applications
SP - 268
EP - 273
BT - 17th IEEE International Conference on Control Applications, CCA
T2 - 17th IEEE International Conference on Control Applications, CCA
Y2 - 3 September 2008 through 5 September 2008
ER -