CourseAerospace, UAM, Drones & Space Applications open

Electric propulsion course for UAVs

Online course of 300 hours in electric propulsion for UAVs: 6 modules covering drone propulsion systems, motors and ESCs, propellers and rotors, energy sources, integration, control and reliability, and a UAV propulsion project, with an assigned technical tutor.

Duration300 hours · 3 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute certificate
Virtual lab · try it before you enrol

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Learning outcomes

What you will be able to do

01

Understand the architecture of a drone electric powertrain.

02

Select motors and ESCs from their characteristic curves.

03

Design and select propellers using blade element theory.

04

Size battery systems and alternative energy sources.

05

Integrate propulsion with the flight controller and its failure logic.

06

Apply European regulatory requirements for drones.

07

Design the complete propulsion system of a UAV for a specific mission.

Profile

Who it's for

  • UAV systems engineers.
  • Electric propulsion engineers moving into unmanned aviation.
  • Drone designers.
  • Drone flight test engineers.
  • UAS maintenance technicians.
  • Payload integration engineers.
  • Engineering or science graduates looking to join the unmanned aviation sector.
Standards & tools

What you'll work with

  • Implementing Regulation (EU) 2019/947 (rules and procedures for the operation of unmanned aircraft)
  • Delegated Regulation (EU) 2019/945 (unmanned aircraft systems and third-country operators)
  • EASA SC Light-UAS (special condition for light unmanned aircraft systems)
  • JARUS SORA 2.5 (specific operations risk assessment)
  • ASTM F3298-19 (design, construction and verification of lightweight UAS)
  • IEC 62133-2:2017 (safety of portable lithium cells and batteries)
  • UN Manual of Tests and Criteria, Section 38.3 (lithium battery transport testing)
  • eCalc
  • PX4 Autopilot
  • ArduPilot Mission Planner
  • XFOIL
  • QPROP
Syllabus

6 modules

  1. 1.1Components of the electric powertrain
  2. 1.2Multirotor, fixed-wing and VTOL configurations
  3. 1.3Thrust requirements and thrust-to-weight ratio
  4. 1.4Endurance and range by configuration
  5. 1.5Open, specific and certified categories
  6. 1.6Drone classes C0 to C6
  7. 1.7Civil applications and their mission profiles
  8. 1.8Trends in drone propulsion
  9. 1.9Component selection criteria
  10. 1.10Case study: analysis of a commercial inspection drone
  1. 2.1Outrunner brushless motors
  2. 2.2KV constant and torque
  3. 2.3Copper and iron losses
  4. 2.4Electronic speed controllers (ESCs)
  5. 2.5Trapezoidal commutation and FOC control
  6. 2.6DShot and PWM protocols
  7. 2.7ESC telemetry
  8. 2.8Motor thermal management
  9. 2.9Motor and propeller test bench
  10. 2.10Lab: performance curve of a motor–propeller set
  1. 3.1Momentum theory
  2. 3.2Blade element theory
  3. 3.3Thrust and power coefficients
  4. 3.4Diameter and pitch selection
  5. 3.5Folding and variable-pitch propellers
  6. 3.6Ground effect and coaxial rotor effects
  7. 3.7Noise of small propellers
  8. 3.8Propeller materials and balancing
  9. 3.9Design with open-source tools
  10. 3.10Workshop: designing a propeller using blade element theory
  1. 4.1LiPo and Li-ion batteries for drones
  2. 4.2Capacity, C-rate and internal resistance
  3. 4.3Series–parallel cell configuration
  4. 4.4Battery management and state of charge
  5. 4.5Hybrid systems with combustion engines
  6. 4.6Fuel cells for long endurance
  7. 4.7Safe transport and storage
  8. 4.8Battery ageing and retirement
  9. 4.9Energy reserve requirements
  10. 4.10Practical exercise: sizing a battery for a mapping mission
  1. 5.1Overall powertrain sizing
  2. 5.2PX4 and ArduPilot flight controllers
  3. 5.3Motor mixing and allocation
  4. 5.4Behaviour after a motor failure
  5. 5.5Electromagnetic compatibility with avionics
  6. 5.6Data logging and flight analysis
  7. 5.7Motor and propeller maintenance
  8. 5.8SORA requirements for propulsion
  9. 5.9Design for the certified category
  10. 5.10Case study: log analysis after a motor failure
  1. 6.1Drone mission and requirements
  2. 6.2Aircraft configuration
  3. 6.3Motor and ESC selection
  4. 6.4Propeller design or selection
  5. 6.5Energy system sizing
  6. 6.6Endurance and performance estimation
  7. 6.7Validation on a test bench or in simulation
  8. 6.8Operational risk analysis
  9. 6.9Report and presentation
  10. 6.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

A 100% online programme on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within each intake, so you can combine it with your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is eCalc, PX4 Autopilot, ArduPilot Mission Planner, XFOIL and QPROP, in free, academic or evaluation versions. Testing is studied through real procedures for bench testing motor–propeller sets, sizing batteries for mapping missions and analysing flight logs after failures. Assessment is continuous by module, plus the final project.

Standards covered: Implementing Regulation (EU) 2019/947, Delegated Regulation (EU) 2019/945, EASA SC Light-UAS, JARUS SORA 2.5, ASTM F3298-19, IEC 62133-2:2017, UN Manual of Tests and Criteria, Section 38.3

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of Regulation (EU) 2019/947, Regulation (EU) 2019/945, EASA SC Light-UAS and JARUS SORA 2.5 applied to real cases, not as a theoretical annex.
Industry software:eCalc, PX4 Autopilot, ArduPilot Mission Planner, XFOIL, QPROP, in free, academic or evaluation versions.
Final project:complete propulsion system of a UAV for a specific mission, from motor, ESC and propeller selection to energy sizing and bench or simulation validation, reviewed by your tutor.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Define the mission
Set the drone mission and requirements and choose the aircraft configuration.
Select motor and ESC
Choose the motor and ESC from their characteristic curves for the required thrust.
Design the propeller
Design or select the propeller using blade element theory.
Size the energy system
Size the battery or hybrid system and estimate endurance and performance.
Final project
Validate on a bench or in simulation, analyse operational risks and present a report reviewed by your tutor.
Career opportunities

Where this takes you

UAV Systems EngineerElectric Propulsion EngineerDrone DesignerDrone Flight Test EngineerUAS Maintenance TechnicianPayload Integration Engineer
Admissions & scholarships

Requirements

  • No prior qualification is required.
  • Internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 300 hours over 3 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with eCalc, PX4 Autopilot, ArduPilot Mission Planner, XFOIL, QPROP, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute certificate, awarded on passing the continuous assessment and the final project. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed are recognised in a higher programme in the same area (postgraduate diploma or master's). Ask about the recognition policy when you enrol.

No prior qualification is required: you need an internet connection, a computer able to run the programme software and English sufficient to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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