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For complete official details and documentation, visit the ISRO IRoC-U2025.


IRoC-U 2025 – Technical Challenge Summary

Challenge Overview

Design and demonstrate an Autonomous Navigation System for an Aerial Vehicle (ANAV) that can function in a simulated Martian environment without any external navigation aids like GNSS, pseudolites, or reflectors.

Core Objectives:

  • Execute fully autonomous:

    • Vertical take-off
    • Terrain-based navigation
    • Safe-spot detection and landing
    • Return to home base
  • Navigation must rely solely on surface topography, not color or beacons.

  • Participants will not build the drone — they may use off-the-shelf rotorcrafts that meet DGCA regulations.


Arena Layout

Arena Layout Arena Layout

30 ft × 40 ft challenge arena with 1 ft yellow boundary.

The arena is designed to emulate Martian terrain using non-uniform, unstructured, and non-color-dependent topography, testing the drone’s ability to perceive, plan, and execute autonomous act

Arena Specifications:
  • Dimensions: 30 ft × 40 ft (approx. 9.1 m × 12.2 m)
  • Boundary: 1 ft wide yellow strip running along all edges for visual demarcation
  • Flight Altitude: Min. 3 m; Max 6 m
  • Enclosure: Optional netting around arena perimeter
Home Position & Landing Zones:
  • Home Pad: 4 ft × 4 ft flat platform at a fixed corner of the arena

  • Safe Landing Zones: Two or more 5 ft × 5 ft areas located within the arena

    • At least one will have an inclined 15° slope
    • Participants must demonstrate slope landing stability
Terrain Composition:

To mimic Martian surface irregularities, the arena floor will include:

  • Loose sand and fine gravel
  • Medium-sized pebbles and thermocol to simulate loose top layer
  • Embedded boulders and raised undulations (1.5 ft to 2.5 ft high)
  • Uneven terrain distribution, forcing real-time mapping and adaptation

The surface is not level. Drones will need to dynamically identify flat areas for landing using onboard sensors, not rely on color, GPS, or any pre-mapped coordinates.


Technical Requirements

ANAV System Specifications
ParameterRequirement
Aerial Vehicle TypeRotorcraft / Micro Drone, Mass < 2 kg
SoftwareNavigation and control algorithms must be developed in-house
Power SourceBattery-operated only
CommunicationRF-based only
Emergency ModeMandatory safe-landing feature on emergency trigger
Slope HandlingMust land safely on slopes of at least 15°
DGCA ComplianceMust follow DGCA rules

Challenge Tasks

Common Across All Rounds
  • Stable vertical take-off (3–10 m hover)
  • Maintain hover for ≥30 seconds
  • Arena scan and boundary detection
  • Identify ≥1.5 m² safe landing zones
  • Land at multiple safe spots
  • Return to home location
  • Real-time telemetry: X, Y, Z, velocities, battery, and safe-spot coordinates

ModeDescription
Manual ModeControlled via base station (e.g., laptop/controller)
AutonomousExecutes navigation tasks autonomously on command
Safe ModeAutomatically activated on emergencies (e.g., low battery, signal loss)

Challenge Rounds

1. Preliminary Round
  • Submit proposal (≤15MB) outlining:

    • Concept
    • Technical approach
    • Innovation
  • Proposal score: 10/100 (rest to be announced)

  • Only 1 team per institute, with HoI approval


2. Qualification Round
Tasks:
  • Take-off from 1.2 m × 1.2 m home location
  • Hover at 3–10 m height for ≥30 sec
  • Land within the same zone
  • Demonstrate emergency-safe landing
Deliverables:
  • HD videos with clear timestamps
  • Complete ANAV design documentation
  • Recordings must be at the institution site

3. Elimination Round
  • Arena: 30 ft × 40 ft, bordered by 1 ft yellow strip

  • Home Pad: 4 ft × 4 ft flat surface

  • Landing Zones: 5 ft × 5 ft, at least one with 15° slope

  • Terrain: Uneven with 1.5–2.5 ft high undulations made from:

    • Sand
    • Gravel
    • Thermocol
    • Small boulders
  • Netting around arena is optional

  • Flight altitude: Minimum 3 m (upper bound unspecified)


4. Field Round (URSC Bengaluru)
  • Same configuration as Elimination Round
  • Added requirement: Return to original home zone after final landing

Glossary

TermDefinition
Home PositionInitial 1.5 m² area where drone starts and must return
Safe Spot≥1.5 m² flat zone with slope <15° for safe landing
Base StationManual control system (typically a laptop/controller)
TelemetryReal-time data: position, height, velocities, battery, and safe-spot coordinates

Prohibited & Mandatory Rules

  • No GNSS, reflectors, pseudolites, or external positioning systems
  • Must comply with DGCA and Ministry of Civil Aviation rules
  • Only the first team per institute will be accepted into the competition