Missile Misdistance Reduction: An Instructive Methodology for Developing Terminal Guidance Control Systems to Minimize Missile Misdistance

摘要

The present thesis is an instructive methodology for developing and improving guidance control systems, in order to minimize the missile misdistance. The complexity of the system which is under development depends heavily upon the defined assumptions, scenarios, specifications, current technology and cost effectiveness. It depends on the designer or the expert, to weight up the advantages and disadvantages of all the above, according to their availability, for obtaining best results. (Author)