CNG course in satellites
About our
The GNC in Satellites course focuses on the design and analysis of guidance, navigation, and control (GNC) systems for space missions. It covers everything from the fundamentals of orbital dynamics and orbit attitude and control to the implementation of advanced control algorithms and the simulation of complex scenarios. sensor and actuator techniques, signal processing, and robust control, essential for the precise operation of satellites and space probes, are explored.
The course offers hands-on training in the use of specialized simulation software and in the validation of GNC systems through testing and validation. Participants will acquire knowledge in mission planning and the management of in-flight anomalies, preparing them for professional roles in the space industry, including GNC engineers, systems analysts, and mission control specialists, covering the needs of the space industry and space exploration.
CNG course in satellites
- Format: Hybrid
- Duration: 3 months
- Hours: 300 H
- Language: English / Spanish
- Registration date: 23-10-2026
- Start date: 12-12-2026
- Available places: 3
349 $
Competencies and results
What you will learn
1. Satellite Attitude and Orbit Control: Fundamentals and Applications GNC
- Fundamental Principles of Attitude and Orbit Control (AOC): Understand the key concepts that govern the orientation and position of satellites in space.
- Orbital Dynamics: Master the crucial aspects of orbital mechanics, including trajectory, perturbation, and orbit prediction.
- Sensors and Actuators: Explore the different types of sensors (solar sensors, star sensors, gyroscopes, accelerometers) and actuators (reaction wheels, thrusters) used in AOC.
- Satellite Modeling: Learn to model the dynamics of a satellite, including its structure, mass, moment of inertia, and the external forces acting upon it.
- Attitude Control: Design and analyze control strategies to orient the satellite in the desired direction, using classical and modern control algorithms.
- Orbit Control: Develop techniques for manipulating satellite orbit, such as orbital corrections, orbit transfers, and collision avoidance.
- Navigation Systems: Study GPS-based navigation systems and other global positioning systems, and how they are integrated into GNC.
- Simulation and Validation: Use simulation tools to evaluate the performance of GNC systems and validate designs.
- GNC Applications: Examine GNC applications in various space missions, such as Earth observation, communications, space exploration, and scientific research.
- Practical Aspects and Design: Learn about the design, testing, and operational challenges of GNC systems in the space environment, including component selection and uncertainty management.
2. In-depth knowledge of the design and performance of rotors in CNG satellite systems
- In-depth analysis of rotor vibration modes, including the identification and mitigation of critical phenomena such as flap-lag-torsion, ensuring the dynamic stability of the system.
- Study advanced techniques for rotor stability and performance analysis, with special emphasis on whirl flutter prevention, crucial for structural integrity and operational safety.
- Evaluate fatigue mechanisms in rotors, applying predictive models to estimate service life and optimize designs for greater durability and reliability.
- Master the dimensioning of composite structures, including material selection, thickness calculations, and optimization of layer arrangement to maximize strength and minimize weight.
- Design and analyze joints in structures
- Analyze composite structures, considering different types of joints (bolted, bonded, etc.) and evaluating their load-bearing capacity and behavior under different loading conditions.
- Implement finite element (FE) analysis to model and simulate the behavior of bonded joints, allowing for a precise evaluation of stresses and strains in bonded joints and optimizing the design for greater efficiency.
- Apply the principles of damage tolerance, including the evaluation of crack propagation and the determination of the remaining service life of structures, to ensure the safety and reliability of the satellite system.
- Use non-destructive testing (NDT) methods, such as ultrasonic testing (UT), radiography (RT), and thermography, to inspect and evaluate the integrity of structures and detect possible defects or damage.
- Interpret the results of the inspections NDT, identify the types of damage and their impact on structural integrity, and make informed decisions about repairs or component replacement.
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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. Advanced Rotor Analysis: Modeling and Performance Evaluation in Satellite CNG Systems
- Modeling and simulation of complex rotors for satellite CNG systems.
- Evaluation of the aerodynamic and structural performance of rotors under various operating conditions.
- Study of advanced aeroelastic phenomena such as flap-lag-torsion, crucial for rotor stability.
- Analysis of whirl flutter, identifying and mitigating instability risks.
- Investigation of structural fatigue and design for rotor durability.
- Application of Finite Element (FE) techniques for the dimensioning of laminates in composites.
- Design and analysis of bonded joints and connections in composite materials.
- Implementation of damage tolerance strategies for damage detection and management.
- Application of testing methods Non-Destructive Testing (NDT), including UT/RT/thermography, for rotor inspection.
5. Modeling and Analysis of Rotor Performance in Satellite CNG Systems
5. Modeling and Analysis of Rotor Performance in Satellite CNG Systems
- Master rotor modeling in satellite CNG systems, including understanding their operation and key variables.
- Acquire skills in simulating rotor dynamics, considering aerodynamic and structural effects.
- Apply finite element analysis (FEA) techniques to evaluate rotor behavior under various operating conditions.
- Learn to optimize rotor design to improve the performance, stability, and energy efficiency of CNG systems.
- Evaluate the impact of manufacturing tolerances and defects on rotor performance.
- Develop skills for detecting and mitigating vibration and resonance problems in rotors.
- Understand the principles of uncertainty management in rotor analysis and how it affects decision-making. Design.
Study case studies of real-world applications of rotors in satellite CNG systems.
Become familiar with the relevant regulations and standards for rotor design and manufacturing.
Learn to use specialized software for rotor modeling and analysis.
6. Modeling and Simulation of Rotor Performance for Satellite CNG
6. Modeling and Simulation of Rotor Performance for Satellite CNG
- Understand and evaluate the crucial aeroelastic couplings in rotor design: flap-lag-torsion, fundamental for stability and dynamic response, and whirl flutter, a high-speed instability phenomenon.
- In-depth analysis of structural fatigue to predict rotor lifespan and ensure operational safety.
- Master finite element (FE) modeling techniques for the precise dimensioning of laminated structures in composites, optimizing strength and weight.
- Design and analyze joints and bonded joints using FEA to ensure structural integrity and efficient load transfer.
- Apply damage tolerance principles to evaluate the rotor’s ability to withstand damage and continue operating. safely.
- Know and apply non-destructive testing (NDT) methods such as Ultrasonic Testing (UT), Radiography (RT), and Thermography for rotor inspection.
Who this program is for:
CNG course in satellites
- 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 GNC: Fundamental Concepts and Terminology
1.2 Orbital Dynamics: Key Principles and Equations
1.3 Attitude and Attitude Control: Definitions and Basic Methods
1.4 Satellite Sensors: Types, Operation, and Applications
1.5 Actuators: Reaction Wheels, Thrusters, and Gyroscopes
1.6 Control Systems: Controller Structure and Design
1.7 GNC Applications: Navigation, Attitude Control, and Orbit Control
1.8 Estimation Fundamentals: Kalman Filters and Estimation Techniques
1.9 GNC Software: Tools and Simulations for Design
1.10 Case Study: Implementing GNC on a Real Satellite
2.2 Fundamentals of Rotor Design for Satellite CNG
2.2 Key Parameters and Rotor Selection
2.3 Aerodynamic and Dynamic Modeling of the Rotor
2.4 Rotor Materials and Manufacturing Technologies
2.5 Rotor Control System Design
2.6 Rotor Integration with the Satellite CNG System
2.7 Rotor Performance Simulation
2.8 Rotor Testing and Validation
2.9 Maintenance and Operation Considerations
2.20 Case Studies: Rotor Design in Satellite Missions
3.3 Fundamentals of Rotor Optimization for Satellite CNG
3.2 Rotor Design: Performance Considerations and Limitations
3.3 Rotor Materials and Manufacturing: Impact on Optimization
3.4 Aerodynamic and Structural Analysis of Rotors: Methods and Tools
3.5 Rotor Modeling and Simulation: Software and Techniques
3.6 Control Algorithms and Their Impact on Rotor Optimization
3.7 Design of Rotor-Based Attitude Control Systems
3.8 Multi-Objective Optimization for Rotors: Performance and Efficiency
3.9 Rotor Testing and Validation: On the Ground and in Orbit
3.30 Case Studies: Rotor Optimization in Specific Satellite Missions
4.4 Introduction to GNC (Guidance, Navigation, and Control) Systems for Satellites
4.2 Fundamentals of Orbital Dynamics and Attitude Control
4.3 Sensors and Actuators for Attitude Control: Types and Principles
4.4 Mathematical Modeling of Satellites and Their Environments
4.5 Basic Design of Control Algorithms for Attitude and Orbit
4.6 Applications of GNC Systems in Space Missions
2.4 Design Principles of Rotors for Satellite Attitude Control
2.2 Selection of Materials and Rotor Configurations
2.3 Aerodynamic Modeling of Rotors
2.4 Design of Rotor Control Systems
2.5 Integration of Rotors into the GNC Subsystem
2.6 Design Considerations for Space Environments
3.4 Key Design Parameters for Rotor Optimization
3.2 Multiobjective Optimization Techniques Applied to Rotors
3.3 Sensitivity Analysis and Tolerances in Design
3.4 Optimization of Mass Distribution and Moments of Inertia
3.5 Optimization of Energy Consumption and Durability
3.6 Implementation of Optimization Algorithms in Rotor Design
4.4 Advanced Rotor Modeling: Methods and Tools
4.2 Analysis of Rotor Frequency Response
4.3 Evaluation of Control Stability and Robustness
4.4 Simulation of Rotor Performance in Different Scenarios
4.5 Analysis of Rotor Failures and Failure Modes
4.6 Validation and Verification of Rotor Design
5.4 Modeling Rotor Dynamics: Equations and Simplifications
5.2 Modeling of Disturbances and External Forces
5.3 Modeling of Sensor Errors and Actuators
5.4 Rotor-Structure Interaction Simulation
5.5 Rotor Performance Evaluation Under Different Operating Conditions
5.6 Model Validation and Comparison with Experimental Data
6.4 Introduction to Simulation Tools for CNG Systems
6.2 Attitude Control Simulation with Rotors
6.3 Orbital Propagation and Orbit Control Simulation
6.4 Rotor Performance Simulation in Different Missions
6.5 Sensitivity Analysis and Case Studies
6.6 Visualization and Analysis of Simulation Results
7.4 Stability and Controllability Analysis in Attitude Systems
7.2 Advanced Control Techniques Applied to Rotors
7.3 Optimization of Control Algorithms for Rotors
7.4 Design Considerations to Minimize Energy Consumption
7.5 Performance Analysis in the Presence of Disturbances
7.6 Design of Fault-Tolerant Attitude Systems
8.4 Performance Metrics for Satellite CNG Systems
8.2 Evaluation of Rotor Performance in Different Scenarios
8.3 Robustness and Disturbance Sensitivity Analysis
8.4 Design of Experiments and Statistical Analysis
8.5 Comparative Evaluation of Different Rotor Configurations
8.6 Conclusions and Recommendations for the Design of CNG Systems
5.5 Introduction to Rotor Modeling for Satellite CNG
5.5 Mathematical and Physical Foundations of Rotor Modeling
5.3 Rotor Dynamics Modeling: Equations and Parameters
5.4 Simulation Techniques for Rotor Performance
5.5 Modeling of Disturbances and Environmental Effects
5.6 Sensitivity and Robustness Analysis of the Model
5.7 Validation and Verification of the Rotor Model
5.8 Applications of Rotor Modeling in CNG Design
5.9 Tools and Software for Rotor Modeling
5.50 Case Studies: Practical Applications and Results
6.6 Introduction to Rotor Simulation for Satellite CNG
6.2 Mathematical Modeling of Rotors for Simulation
6.3 Rotor Dynamics Simulation: Software and Tools
6.4 Implementation of CNG Algorithms in Rotor Simulations
6.5 Results Analysis: Interpretation of Simulation Data
6.6 Validation and Verification of Simulation Models
6.7 Simulation of Operational Scenarios: Failures and Contingencies
6.8 Optimization of Design Parameters through Simulation
6.9 Integration of Simulations with Development Environments
6.60 Case Studies: Practical Applications of Simulation
- 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
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”).