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Inertial Navigation System (INS) is required for implementing point to coordinate and target coordinate calculation. INS is used to update the position of Gimbal Payload Assembly (GPA) in three dimensional space.INS will provide accurate attitude, position and velocity of the system.INS shall be of light weight and shall be in small size to accommodate with in the gimbal assembly. Micro Electro Mechanical System (MEMS) based Attitude Heading Reference System (AHRS) and related processingdoi:10.5120/6372-8798 fatcat:3ymqkpj2dbg4dc7w2lqrgaud54