#TITLE_ALTERNATIVE#

• Main Author: MEDI HUTAMA PUTRA (NIM : 13613075), ICHSAN
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/27905
• Institution: Institut Teknologi Bandung

Fighter maneuvers developed over the years for the benefit of air combat. One of its uses is as a way of avoiding missile attacks launched by enemy combat aircraft (or commonly referred to as evasive maneuvers). This Final Project will discuss the effectiveness of Immelmann Turn and Split-S evasive maneuvers in its usefulness to avoid missile attacks launched by enemy combat aircraft. The effectiveness of the maneuver itself depends on the position of the fighter and the direction of the missile attack. The effectivity level is measured from a parameter called miss distance. To provide the miss distance, the engagement simulation between missile and maneuverable target will be done. The SIMULINK software is used to build dynamic models of combat aircraft, so that the resulting trajectory of maneuver can be analyzed. In addition, this software is also used to implement the motion equation of missile with Proportional Navigation guiding system, then simulated with various engagement geometry to obtain miss distance. Then, the distribution of miss distance and the area where the missile can hit the fighter (kill area) will be evaluated. There are several variations of scenarios including the variation of missile line-of-sight distance and the variation of maximum turn rate of the missile. The miss distance result from engagement simulation between missiles and maneuvering target will be compared to see how effective the maneuvers are.