SIH26098HardwareSmart Vehicles
₹1,50,000 Prize (₹75k Joint)
•
Deadline: 20 September 2026
•
Submitted Ideas: 0/500

Development of a Low-Cost Precision Guidance and Smart Electronic Fuze System for a 155 mm Artillery Shell

Ministry / Organization: Ministry of Defence (MoD)
Department: Yantra India Limited, Ambajhari,Nagpur
Technical Complexity
9/10
Dataset Accessibility
5/10
36h Hackathon Viability
6/10
Step 0 • Zero-Jargon Layman Summary

“You are building a 'smart kit' that attaches to standard artillery shells to make them hit targets with pinpoint accuracy. It uses tiny wings to steer the shell in mid-air and a smart electronic brain to decide exactly when and how to explode.”

The DecodeX PS Decoder™

Deconstructed Problem Blueprint

Step 1

WHAT TO BUILD?

A modular Precision Guidance Kit (PGK) consisting of a Canard Actuation Assembly (CAA) for steering and a Multi-mode Electronic Fuze for detonation control.

Step 2

WHO IS IT FOR?

Yantra India Limited (YIL) and the Indian Army artillery units. The end-users are artillery gunners and field commanders.

Step 3

WHY DOES IT EXIST?

Standard artillery shells are 'dumb' projectiles that drift significantly over long distances, leading to wasted ammunition and high collateral damage. Precision guidance reduces the number of shells needed to neutralize a target.

Step 4

INPUT → PROCESS → OUTPUT ARCHITECTURE PIPELINE

01 • Inputs & Telemetry

GPS/GNSS coordinates, IMU (accelerometer/gyroscope) data, barometric pressure, and pre-fire mission parameters (target coordinates, fuse mode).

02 • Processing & AI Core

Real-time trajectory calculation, PID/LQR control loop for canard actuation, high-g sensor fusion, and fuze logic processing.

03 • Actionable Deliverables

Physical movement of canard fins for steering, detonation signal for the fuze, and telemetry data for post-mission analysis.

Step 5

CONSTRAINTS

  • Must survive 15,000g+ launch acceleration.
  • Must operate under high-spin conditions (up to 250 RPS).
  • Must fit within the standard 155mm shell nose cone volume.
  • Must be low-cost for mass production.
  • Must be immune to electronic jamming/spoofing.
Step 6

JURY METRICS

  • Circular Error Probable (CEP) <= 30 meters.
  • System latency (time from sensor input to fin actuation).
  • Power efficiency (battery life during flight).
  • Structural integrity under high-g simulation.
  • Cost-per-unit vs. conventional unguided shell.
Step 7

CORE BOTTLENECK

The 'High-g' survival requirement: Designing electronics and mechanical actuators that don't shatter or fail under the extreme force of a cannon launch.

Why You Should Choose This PS (Pros)

  • High national security impact.
  • Clear, hardware-focused engineering challenge.
  • Strong potential for patent filing.
  • Direct alignment with 'Atmanirbhar Bharat' defense initiatives.

Challenges & Risks to Watch (Cons)

  • Extremely difficult to prototype physically in 36 hours.
  • Requires advanced knowledge of control theory and aerospace dynamics.
  • High risk of simulation failure if physics models are inaccurate.
Hackathon Blueprint

Recommended Tech Stack & Grand Finale Features

Frontend & Mobile
React.js for the Mission Planning Dashboard
Backend & APIs
Python for GNC algorithm prototyping
AI / ML & Models
PID/LQR Control AlgorithmsKalman Filters for Sensor Fusion
Database & Cloud
SQLite for flight log storage

Killer Features to Impress the SIH Jury

Anti-jamming GNSS logic using inertial dead-reckoning fallback.
Modular 'plug-and-play' design that fits existing shells without modification.
Fail-safe 'Safe-to-Arm' logic that prevents premature detonation.
Digital Twin simulation showing trajectory correction in real-time.
View Official SIH 2026 Portal Raw Text
▼
•Problem Title Design and Development of a Precision Guidance Kit with Canard Actuation and Multi-Mode Electronic Fuze for a 155 mm Artillery Shell
•Background Conventional 155 mm artillery shells rely on unguided ballistic trajectories, resulting in relatively high Circular Error Probable (CEP), particularly at long ranges. Improving strike accuracy while utilizing existing shell hardware can significantly enhance operational effectiveness, reduce ammunition consumption, and minimize collateral damage.

The YIL (Yantra India Limited) possesses extensive expertise in manufacturing the mechanical hardware of 155 mm artillery shells and seeks innovative solutions to transform conventional shells into precision-guided munitions through the integration of an advanced guidance and fuze system.

•Problem Statement Develop a compact, robust, and cost-effective precision guidance solution for a standard 155 mm artillery shell by integrating:
•A Canard Actuation Assembly (CAA) for in-flight trajectory correction.
•A Guidance,Navigation and Control (GNC) system capable of improving terminal accuracy.
•A Multi-mode Electronic Fuze supporting:
•Proximity Mode
•Time Mode
•Impact Mode
•Embedded electronics and software for real-time flight control.
•Power management suitable for high-g launch and flight conditions.
•Communication and programming interface for fuze configuration prior to firing.

The integrated system should achieve a Circular Error Probable (CEP) of 30 meters or better, while maintaining compatibility with the existing 155 mm shell design and surviving the extreme mechanical and environmental conditions experienced during artillery launch and flight.

•Expected Outcome Participants should propose a complete system architecture including:
•Guidance and navigation methodology.
•Canard deployment and actuation mechanism.
•Flight control algorithms.
•Multi-mode electronic fuze design.
•Sensor selection (e.g., IMU, GNSS, barometric sensor, proximity sensor, etc.).
•Embedded hardware architecture.
•Power supply and environmental protection strategy.
•Simulation and validation methodology.
•Manufacturability and cost optimization.
•Desired Deliverables
•System architecture document.
•CAD model of the canard actuation assembly.
•Electronics block diagram.
•Guidance and control algorithm.
•Simulation demonstrating trajectory correction.
•Prototype or proof-of-concept (preferred).
•Performance estimation showing the capability to achieve a CEP of ?30

m.

•Constraints
•Compatible with a standard 155 mm artillery shell casing.
•Must withstand high launch acceleration, vibration, spin, and harsh environmental conditions.
•Low Size, Weight, Power, and Cost (SWaP-C).
•High reliability and safety.
•Modular design suitable for future upgrades.
•Skills Expected from Participants
•Mechanical Design
•Mechatronics
•Embedded Systems
•Control Systems
•Guidance, Navigation & Control (GNC)
•Aerospace Engineering
•Electronics