Satellite attitude course
About our
The Satellite Attitude Course explores the principles of satellite orientation and control, covering everything from theory to practical implementation. It delves into satellite dynamics, the design of sensors and actuators, and the control algorithms used to maintain precise orientation in space. It focuses on modeling and simulation of attitude control systems, including the handling of external perturbations such as gravitational gradient and atmospheric drag. The training prepares professionals for roles in satellite systems design, mission control, and telemetry data analysis, with a focus on the reliability and accuracy of space operations. The course includes case studies and simulations for sensor calibration, noise and drift analysis, and the implementation of robust attitude control strategies. Attitude determination techniques using sensors such as gyroscopes, accelerometers, solar and star sensors, as well as actuators such as reaction wheels and thrusters, are reviewed. The course emphasizes the application of this knowledge to the design of attitude control subsystems, performance optimization, and the planning of successful space missions.
Satellite attitude course
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
275 $
Competencies and results
What you will learn
1. Satellite Attitude and Control: Comprehensive Mastery
- Understand satellite attitude: orientation in space.
- Master attitude control: control systems, actuators, and sensors.
- Analyze satellite dynamics: equations of motion, perturbations, and stability.
- Study orbit: orbit types, orbital elements, and maneuvers.
- Implement control algorithms: PID control, sliding mode control, and optimal control.
- Analyze power management: solar panels, batteries, and power distribution.
- Become familiar with telemetry, tracking, and control (TT&C).
- Understanding satellite operations: launch, commissioning, and mission management.
2. Modeling, Simulation and Performance of Propellers
- In-depth analysis of critical structural phenomena in propellers, including flap-lag-torsion couplings, which affect stability and dynamic behavior.
- Evaluate susceptibility to whirl flutter, a detrimental vibration mode, and develop strategies to mitigate it.
- Study fatigue mechanisms and their impact on propeller lifespan, applying design criteria to increase durability.
- Apply finite element (FE) modeling techniques to dimension laminates in composites, optimizing strength and weight.
- Design and analyze structural joints, including bonded joint methods, to ensure integrity and effective load transfer.
- Understand the importance of material selection and Layer configuration in the manufacture of composite propellers.
Integrate the damage tolerance (DTT) philosophy into propeller design, considering damage scenarios and establishing safety limits.
Apply NDT (Non-Destructive Testing) techniques, such as ultrasonic testing (UT), radiography (RT), and thermography, for the inspection and evaluation of propellers.
Interpret NDT results to identify defects, evaluate structural integrity, and ensure compliance with quality standards.
3. Comprehensive user-oriented design and validation (from modeling to manufacturing)
You will learn to integrate the entire product development process, from initial model conception to final validation, applying user-centered methodologies. You will develop skills in parametric design, ergonomics, simulation, sustainable materials, 3D visualization, and manufacturing management, ensuring efficient, safe solutions that meet current industry standards.
4. Satellite Attitude: Deep Learning
- Analyze flap–lag–torsion couplings, whirl flutter and fatigue.
- Size laminates in composites, unions and bonded joints with FE.
- Implement damage tolerance and NDT (UT/RT/thermography).
5. Satellite Attitude: Practical and Applied Learning
- Master satellite attitude assessment, including understanding and analyzing attitude control systems (ACS).
- Learn to identify and troubleshoot problems related to satellite stability and performance.
- Acquire practical skills in calibrating and optimizing satellite sensors and actuators.
- Become familiar with key concepts of satellite navigation and precise positioning.
- Understand the fundamentals of satellite telemetry, tracking, and control (TT&C).
- Apply knowledge to satellite attitude simulations and modeling using specialized software.
- Learn about different satellite missions and their specific attitude requirements.
- Develop problem-solving and decision-making skills in attitude control scenarios.
- Understand the safety and The reliability of satellite attitude control systems.
Explore the latest trends and technologies in the field of satellite attitude control.
6. Attitude in Satellites: Fundamentals and Operations
6. Attitude in Satellites: Fundamentals and Operations
- Understand the influence of the moment of inertia and the center of gravity on stability.
- Study attitude control systems: flywheel, gas jets, and sensors.
- Analyze error propagation in attitude determination.
- Learn about star alignment and navigation using satellites.
- Explore the environmental effects (solar radiation, micrometeorites) on attitude.
- Design and simulate satellite maneuvering and orientation strategies.
- Evaluate the performance of attitude sensors: gyroscopes, magnetometers, and solar sensors.
- Implement control algorithms for satellite stabilization and pointing.
- Understand the space regulations and standards related to attitude.
- Apply optimization techniques to improve the efficiency of control systems.
Who this program is for:
Satellite attitude course
- Graduates in Aerospace Engineering, Mechanical Engineering, Industrial Engineering, Automation Engineering, or related fields.
- Professionals in OEM rotorcraft/eVTOL, MRO, consulting, and technology centers.
- Flight Testing, certification, avionics, control, and dynamics seeking specialization.
- Regulators/authorities and UAM/eVTOL professionals requiring compliance skills.
Recommended requirements: foundation in aerodynamics and control and structures; ES/EN B2+/C1. We offer bridging tracks if you need them.
- Standards-driven curriculum: you will work with CS-27/CS-29, DO-160, DO-178C/DO-254, ARP4754A/ARP4761, ADS-33E-PRF from the first module.
- Accreditable laboratories (EN ISO/IEC 17025) with rotor bench, EMC/Lightning pre-compliance, HIL/SIL, vibrations/acoustics.
- Evidence-oriented TFM: safety case, test plan, compliance dossierand operational limits.
- Mentored by industry: teachers with experience in rotorcraft, tiltrotor, eVTOL/UAM and flight test.
- Flexible modality (hybrid/online), international cohorts and support from SEIUM Career Services.
- Ethics and security: safety-by-design approach, cyber-OT, DIH and compliance as pillars.
1.1 Introduction to Satellite Attitude: Definitions and Key Concepts
1.2 Reference Frames: Inertial and Non-Inertial Frames
1.3 Rotational Dynamics: Euler’s Equations and Moments of Inertia
1.4 Attitude Sensors: Types and Operation (Star Sensors, Gyro Sensors, Solar Sensors)
1.5 Attitude Control Actuators: Inertia Wheels, Reaction Flywheels, Control Rockets
1.6 Attitude Controllers: Classical and Modern Control Theory
1.7 Design of Attitude Control Systems: Specifications and Requirements
1.8 Stability and Robustness in Satellite Attitude Systems
1.9 Analysis and Simulation of Attitude Systems
1.10 Fundamentals of Satellite Attitude Operations and Management
2.2 Principles of Propeller Propulsion: Actuator Disk Theory
2.2 Aerodynamic Design of Propellers: Airfoils and Geometry
2.3 Mathematical Modeling of Propellers: Flow Equations and Performance
2.4 Computational Simulation of Propellers: CFD and BEM
2.5 Analysis of Propeller Performance: Thrust, Torque, and Efficiency
2.6 Propeller Selection and Optimization: Criteria and Methodologies
2.7 Effects of Propeller-Flow Interaction: Wake and Cavitation
2.8 Modeling and Simulation of Propellers under Different Operating Conditions
2.9 Experimental Validation of Propeller Models: Wind Tunnel Testing
2.20 Practical Applications of Propeller Modeling and Simulation: Naval Design
3.3 Introduction to Satellite Attitude: Fundamental Concepts
3.2 Orbital Dynamics: Influence on Attitude
3.3 Attitude Sensors: Types and Operation
3.4 Attitude Actuators: Principles and Applications
3.5 Attitude Control: Algorithms and Strategies
3.6 Satellite Stabilization: Common Methods
3.7 Stability Analysis: Techniques and Tools
3.8 Design of the Attitude Control Subsystem (ACS)
3.9 ACS Testing and Validation
3.30 Satellite Attitude Operations and Management
4.4 Fundamentals of Satellite Attitude: Review of key concepts.
4.2 Rotational Dynamics: Analysis of rotational motions.
4.3 Attitude Sensors: Types and operation.
4.4 Attitude Actuators: Principles and applications.
4.5 Attitude Control: Design of control systems.
4.6 Control Algorithms: Implementation and analysis.
4.7 Orbit and Disturbances: Influence on attitude.
4.8 Modeling and Simulation: Tools and techniques.
4.9 Advanced Applications: Orientation and precise control.
4.40 Challenges and Trends: Future of satellite attitude.
5.5 Design and Fundamentals of Satellite Attitude Control
5.5 Sensors and Actuators for Attitude Control
5.3 Orbital Dynamics and Their Influence on Attitude
5.4 Attitude Control Algorithms: Practical Implementation
5.5 Simulation and Performance Analysis of Attitude Control Systems
5.6 Integration and Calibration of Attitude Control Systems
5.7 Testing and Validation of Attitude Control Systems in the Laboratory
5.8 Satellite Attitude in Real-World Operating Scenarios
5.9 Troubleshooting and Failure Analysis in Attitude Control Systems
5.50 Future Trends in Satellite Attitude Control
6.6 Fundamentals of Satellite Attitude
6.2 Space Reference Systems
6.3 Attitude Sensors: Types and Operation
6.4 Attitude Actuators: Types and Operation
6.5 Rotational Dynamics of Rigid Bodies
6.6 Attitude Control: Algorithms and Strategies
6.7 Attitude Operations: Acquisition, Stabilization, and Pointing
6.8 Design of Attitude Systems
6.9 Simulation and Testing of Attitude Systems
6.60 Mission Considerations and Attitude Design
- Hands-on methodology: test-before-you-trust, design reviews, failure analysis, compliance evidence.
- Software (depending on licenses/partners): MATLAB/Simulink, Python (NumPy/SciPy), OpenVSP, SU2/OpenFOAM, Nastran/Abaqus, AMESim/Modelica, acoustics tools, planning toolchains DO-178C.
- SEIUM Laboratories: scale rotor bench, vibrations/acoustics, EMC/Lightning pre-compliance, HIL/SIL for AFCS, data acquisition with strain gauging.
- Standards and compliance: EN 9100, 17025, ISO 27001, GDPR.
Capstone-type projects
- Satellite Design and Control: Attitude and Orbit Integration; Simulation and Validation.
- Propeller Simulation: Modeling and Performance Analysis; CFD Studies.
- Satellite Attitude Systems: Design, Implementation, and Advanced Control.
- Satellite Control: Design and simulation of attitude control algorithms.
- Trajectory Analysis: Modeling and simulation of satellite orbits.
- Attitude Modeling and Simulation: Development of satellite attitude models and simulations.
- Attitude System Evaluation: Comparison of different sensors and actuators.
- Advanced Satellite Control: Implementation of attitude control algorithms (PID, LQR) in 3D simulations, including external disturbances and performance comparison.
- Robust Satellite Control: Design, simulation, and validation of attitude algorithms for complex space missions.
- Advanced Propeller Simulation: CFD modeling, performance optimization, and noise analysis.
- Satellite Guidance System: Implementation of control and navigation algorithms for satellites in orbit.
- Intelligent Satellite Attitude: Development of adaptive attitude control software for satellites.
Admissions, fees, and scholarships
- Profile: Background in Computer Engineering, Mathematics, Statistics, or related fields; practical experience in NLP and valued information retrieval systems.
- Documentation: Updated CV, academic transcript, SOP/statement of purpose, project examples or code (optional).
- Process: Application → Technical evaluation of profile and experience → Technical interview → Review of case studies → Final decision → Enrollment.
- Fees:
- Single payment: 10% discount.
- Payment in 3 installments: No fees; 30% upon registration + 2 equal monthly payments of the remaining 35%.
Monthly payment: available with a 7% commission on the total; annual review.
Scholarships: based on academic merit, financial need, and promoting inclusion; agreements with companies in the sector for partial or full scholarships.
See “Calendar & Calls for Applications,” “Scholarships & Grants,” and “Fees & Financing” in the SEIUM mega-menu.
Do you have any questions?
Our team is ready to help you. Contact us, and we will respond as soon as possible.
F. A. Q
Frequently asked questions
Yes, we have international certification
Yes: experimental models, real data, applied simulations, professional environments, real case studies.
It is not mandatory. We offer leveling tracks and tutoring.
Completely. It covers e-propulsion, integration, and emerging regulations (SC-VTOL).
Recommended. There are also internal challenges and consortiums.
Yes. Online/hybrid modality with planned labs and visa support (see “Visa & Residence”).