PORTALE DELLA DIDATTICA

PORTALE DELLA DIDATTICA

PORTALE DELLA DIDATTICA

Elenco notifiche



FUNDAMENTALS OF SPACE TECHNOLOGY : SYSTEM AND AOCS DESIGN FOR LEO AND GRAVITY MONITORING SATELLITES (didattica di eccellenza)

01HNARV

A.A. 2022/23

Course Language

Inglese

Degree programme(s)

Doctorate Research in Ingegneria Elettrica, Elettronica E Delle Comunicazioni - Torino

Course structure
Teaching Hours
Lezioni 24
Lecturers
Teacher Status SSD h.Les h.Ex h.Lab h.Tut Years teaching
Novara Carlo Professore Ordinario IINF-04/A 2 0 0 0 1
Co-lectures
Espandi

Context
SSD CFU Activities Area context
*** N/A ***    
GUEST LECTURE Luca MASSOTTI EUROPEAN SPACE AGENCY (ESA/ESTEC) Acronyms: AOCS: Attitude and Orbit Control System CMG: Control Moment Gyroscope ESA: European Space Agency EO: Earth Orbit EP: Electric Propulsion GOCE: Gravity field and steady-state Ocean Circulation Explorer GNSS: Global Navigation Satellite System ISS: International Space Station LEO: Low Earth Orbit LISA: Laser Interferometer Space Antenna NGGM: Next Generation Gravity Mission Topics: - Overview of ESA missions, with links to similar non-EU missions (3 hrs) - Sensors for Attitude and Orbital Control Systems (AOCS) (3 hrs) - Propulsion technologies (2 hrs) - Actuators for AOCS (3 hrs) - Gravity Missions: GOCE and MAGIC/NGGM (4 hrs) - Synergies in technology: commonalities between LISA and NGGM (2 hrs) - AOCS design of Earth Explorer LEO satellites (2 hrs) - Geostationary satellites with very high stability requirements (2 hrs) - Exercises and hands on specific space design problems (3 hrs) Part 1: introduction to space missions Overview of ESA missions, with a look at similar non-EU missions (3 hrs) ¿ Presentation of the course and of the speaker ¿ Basic principles of Remote Sensing for EO ¿ Overview of the ESA’s Earth Explorer program, the Sentinel program, the Meteorological program ¿ Non-EU programs ¿ Satellite trivia, Exploration, ISS and launchers EXE 1 (1 hr). General EO satellite design Part 2: Earth observation space missions design AOCS and sensors (3 hrs) ¿ Introduction to the satellite’s attitude and orbit control system (AOCS) ¿ Pointing requirements: analysis and formulation of the requirements ¿ Overview of the sensors for Earth Observation missions and their classification ¿ Inertial sensors (accelerometers and gyroscopes) ¿ Position/navigation sensors (GNSS) ¿ Attitude Sensors (Sun sensors, Earth sensors, star sensors, magnetometers) Actuators for space applications (3 hrs) ¿ Overview of the actuators for Earth Observation missions and their classification ¿ Linear momentum actuators (thrusters) ¿ Angular momentum actuators (momentum wheels, reaction wheels, CMG) ¿ Actuators making use of the planetary magnetic field (magnetic torque rods) Propulsion technologies (2 hrs) ¿ Overview of the propulsion technologies for space ¿ Thermodynamic/chemical thrusters ¿ Cold gas thrusters ¿ Electric propulsion (EP): overview of the technology developments and available products ¿ Examples of EP thrusters: the Indium mN-FEEP and the mini-RIT Gravity Missions: GOCE and MAGIC/NGGM (Next Generation Gravity Mission) (4 hrs) ¿ Objectives and criticalities ¿ Observables and related science products ¿ Brief overview of the gravity missions (EU and US missions) ¿ Measurement principles ¿ The GOCE mission: a close look at the satellite, mission profile and achievements ¿ NGGM: mission and (on-going) satellite design, mission profile, technology status and the NGGM international cooperation scenario EXE 2 (1 hr). Satellite sub/system design Synergies in technology: commonalities between LISA and NGGM (2 hrs) ¿ System and Payload: common elements and driving elements ¿ Actuators enabling both missions AOCS design of Earth Explorer LEO satellites (2 hrs) ¿ Typical observation scenarios for EO ¿ Platform classes and classification ¿ Examples of AOCS design for imager and SAR satellites (e.g. EE7 Biomass) Missions (telecom, weather forecast and security) in GEO orbits (2 hrs) ¿ Applications for telecom, weather forecast and security ¿ A challenging mission: GEO-HR (a geostationary satellite with very high stability requirements) ¿ Introduction to Image and Navigation Registration (INR) EXE 3 (1 hr). LEO/NGGM mission design
GUEST LECTURE Luca MASSOTTI EUROPEAN SPACE AGENCY (ESA/ESTEC) Acronyms: AOCS: Attitude and Orbit Control System CMG: Control Moment Gyroscope ESA: European Space Agency EO: Earth Orbit EP: Electric Propulsion GOCE: Gravity field and steady-state Ocean Circulation Explorer GNSS: Global Navigation Satellite System ISS: International Space Station LEO: Low Earth Orbit LISA: Laser Interferometer Space Antenna NGGM: Next Generation Gravity Mission Topics: - Overview of ESA missions, with links to similar non-EU missions (3 hrs) - Sensors for Attitude and Orbital Control Systems (AOCS) (3 hrs) - Propulsion technologies (2 hrs) - Actuators for AOCS (3 hrs) - Gravity Missions: GOCE and MAGIC/NGGM (4 hrs) - Synergies in technology: commonalities between LISA and NGGM (2 hrs) - AOCS design of Earth Explorer LEO satellites (2 hrs) - Geostationary satellites with very high stability requirements (2 hrs) - Exercises and hands on specific space design problems (3 hrs) Part 1: introduction to space missions Overview of ESA missions, with a look at similar non-EU missions (3 hrs) ¿ Presentation of the course and of the speaker ¿ Basic principles of Remote Sensing for EO ¿ Overview of the ESA’s Earth Explorer program, the Sentinel program, the Meteorological program ¿ Non-EU programs ¿ Satellite trivia, Exploration, ISS and launchers EXE 1 (1 hr). General EO satellite design Part 2: Earth observation space missions design AOCS and sensors (3 hrs) ¿ Introduction to the satellite’s attitude and orbit control system (AOCS) ¿ Pointing requirements: analysis and formulation of the requirements ¿ Overview of the sensors for Earth Observation missions and their classification ¿ Inertial sensors (accelerometers and gyroscopes) ¿ Position/navigation sensors (GNSS) ¿ Attitude Sensors (Sun sensors, Earth sensors, star sensors, magnetometers) Actuators for space applications (3 hrs) ¿ Overview of the actuators for Earth Observation missions and their classification ¿ Linear momentum actuators (thrusters) ¿ Angular momentum actuators (momentum wheels, reaction wheels, CMG) ¿ Actuators making use of the planetary magnetic field (magnetic torque rods) Propulsion technologies (2 hrs) ¿ Overview of the propulsion technologies for space ¿ Thermodynamic/chemical thrusters ¿ Cold gas thrusters ¿ Electric propulsion (EP): overview of the technology developments and available products ¿ Examples of EP thrusters: the Indium mN-FEEP and the mini-RIT Gravity Missions: GOCE and MAGIC/NGGM (Next Generation Gravity Mission) (4 hrs) ¿ Objectives and criticalities ¿ Observables and related science products ¿ Brief overview of the gravity missions (EU and US missions) ¿ Measurement principles ¿ The GOCE mission: a close look at the satellite, mission profile and achievements ¿ NGGM: mission and (on-going) satellite design, mission profile, technology status and the NGGM international cooperation scenario EXE 2 (1 hr). Satellite sub/system design Synergies in technology: commonalities between LISA and NGGM (2 hrs) ¿ System and Payload: common elements and driving elements ¿ Actuators enabling both missions AOCS design of Earth Explorer LEO satellites (2 hrs) ¿ Typical observation scenarios for EO ¿ Platform classes and classification ¿ Examples of AOCS design for imager and SAR satellites (e.g. EE7 Biomass) Missions (telecom, weather forecast and security) in GEO orbits (2 hrs) ¿ Applications for telecom, weather forecast and security ¿ A challenging mission: GEO-HR (a geostationary satellite with very high stability requirements) ¿ Introduction to Image and Navigation Registration (INR) EXE 3 (1 hr). LEO/NGGM mission design
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The course will give an overview on space mission design devoted to Earth Observation (with a special focus on gravity missions), from scientific observables to AOCS design, technology design and qualification aspects, till mission architecture and implementation
The course will give an overview on space mission design devoted to Earth Observation (with a special focus on gravity missions), from scientific observables to AOCS design, technology design and qualification aspects, till mission architecture and implementation
In presenza
On site
Presentazione report scritto
Written report presentation
P.D.2-2 - Maggio
P.D.2-2 - May
Thrursday 18/05 1000 to 1300 hrs Sala riunioni Shannon (3 hrs) Friday 26/05 1200 to 1400 hrs REMOTELY (2 hrs) Wednesday 31/05 1730 to 1830 hrs REMOTELY (1 hrs) Monday 05/06 0930 to 1330 hrs Sala riunioni Shannon (4 hours) Wednesday 07/06 1730 to 1830 hrs REMOTELY (1 hrs) Friday 09/06 1600 to 1800 hrs REMOTELY (2 hrs) Monday 19/06 1800 to 1900 hrs REMOTELY (1 hrs) Friday 23/06 1600 to 1800 hrs REMOTELY (2 hrs) Wednesday 28/06 1700 to 1900 hrs REMOTELY (2 hrs) Friday 30/06 0900 to 1600 hrs Sala riunioni Shannon (6 hours)
Thrursday 18/05 1000 to 1300 hrs Sala riunioni Shannon (3 hrs) Friday 26/05 1200 to 1400 hrs REMOTELY (2 hrs) Wednesday 31/05 1730 to 1830 hrs REMOTELY (1 hrs) Monday 05/06 0930 to 1330 hrs Sala riunioni Shannon (4 hours) Wednesday 07/06 1730 to 1830 hrs REMOTELY (1 hrs) Friday 09/06 1600 to 1800 hrs REMOTELY (2 hrs) Monday 19/06 1800 to 1900 hrs REMOTELY (1 hrs) Friday 23/06 1600 to 1800 hrs REMOTELY (2 hrs) Wednesday 28/06 1700 to 1900 hrs REMOTELY (2 hrs) Friday 30/06 0900 to 1600 hrs Sala riunioni Shannon (6 hours)