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EXAM OVERVIEW

It includes eight modules with a total of 128 questions. Candidates are allowed a maximum of 32 incorrect answers to pass the exam. 

  • Format: Online, proctored exam 

  • Duration: 1.5 hours 

  • Passing Score: 75% (96/128 correct answers) 

The exam assesses candidates on three dimensions of knowledge: 

  • Factual (What): Understanding key concepts and definitions. 

  • Conceptual (Why): Recognizing the importance and reasoning behind practices. 

  • Procedural (How): Applying methods to real-world scenarios 

Exam standards

  • 1.1. Define the principles of missile guidance and control.
    1.2. Explain the difference between open-loop and closed-loop guidance systems.
    1.3. Identify the key components of a missile guidance system:

    • 1.3.1. Sensors and onboard processors.

    • 1.3.2. Actuators and control surfaces.

    • 1.3.3. Navigation and targeting modules.

  • 2.1. Define the role of inertial navigation in missile targeting. 
    2.2. Describe gyroscopes and accelerometers used in INS. 
    2.3. Explain drift errors and methods of correction in INS-based guidance. 
    2.4. Compare strapdown vs. gimbaled inertial navigation systems. 

  • 3.1. Explain the role of GPS in missile navigation and targeting.
    3.2. Describe how GPS augmentation improves missile accuracy.
    3.3. Identify vulnerabilities in GPS-guided systems and countermeasures.
    3.4. Explain integration of multi-constellation GNSS (GPS, Galileo, GLONASS) for redundancy.

  • 4.1. Define terminal guidance and its role in high-precision strikes. 
    4.2. Compare active, semi-active, and passive terminal guidance methods. 
    4.3. Explain seeker technologies used in terminal guidance: 

    • 4.3.1. Radar seekers. 

    • 4.3.2. Infrared (IR) homing systems. 

    • 4.3.3. Electro-optical and laser guidance systems. 

    4.4. Discuss anti-jamming technologies used to protect terminal guidance accuracy. 

  • 5.1. Explain ballistic vs. non-ballistic missile trajectories.
    5.2. Identify factors affecting missile trajectory planning:

    • 5.2.1. Atmospheric drag and wind resistance.

    • 5.2.2. Gravity and Coriolis effects.

    • 5.2.3. Target movement prediction.

    5.3. Discuss mid-course guidance updates and in-flight trajectory adjustments.
    5.4. Explain the role of artificial intelligence in real-time missile guidance.

  • 6.1. Explain how thrust vectoring affects missile maneuverability. 
    6.2. Compare different thrust vector control (TVC) mechanisms: 

    • 6.2.1. Gimbaled nozzles. 

    • 6.2.2. Jet vanes and reaction control systems (RCS). 

    • 6.2.3. Aerodynamic control surfaces. 

    6.3. Identify flight stability challenges and corrective measures. 

  • 7.1. Describe the architecture of missile fire control systems. 
    7.2. Explain sensor fusion techniques for target acquisition. 
    7.3. Discuss the role of command and control (C2) networks in missile operations. 
    7.4. Outline the integration of fire control systems with radar, drones, and other battlefield assets. 

  • 8.1. Discuss AI-driven missile guidance and autonomous targeting. 
    8.2. Explain hypersonic missile guidance challenges and solutions. 
    8.3. Identify future advancements in precision-guided munitions (PGMs). 

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