satellite system design in critical design review phase
SysteDesig
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36 slides
Jul 05, 2024
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About This Presentation
satellite design
Size: 1.35 MB
Language: en
Added: Jul 05, 2024
Slides: 36 pages
Slide Content
Design Procedures
Design Defination
System
<< A set of functional elements organized to satisfy
user needs >> (IEEE P1220)
Mission/Objective
<< Specific task, duty or function defined to be
accomplished by a system >> (EN 13701:2001)
Requirement
<< Need or expectation that is stated, generally
implied or obligatory >> [ISO 9000:2000]
Design Requirements
Process Flow Diagram
Initialize
SGP4
IGRF
SUN
Payload On
Measure
MAG
IMU
Compute
EKF1
EKF2
Estimate
Attitude
Ephemerid
Store Data
Attitude
Ephemerid
Software Process Flow.
Design Requirements
Process Flow Diagram
Operation Process Flow.
1.0
Launch
2.0
Commissioni
ng
[co-proc. is in
good working
order]
3.0
Normal
Operati
on 3.1
MAG
3.2
MAG
3.3 EKF
on
3.4
ADS /
ODS on
3.5
pass /
store
data
3.6
MAG
off
3.2a
Calibrate
MAG
O
K?
N
Y
4.0
Error
4.1
Error
recover
y
4.2
Termina
tion
Design Requirements
CONOPs –Concepts Of Operations
Design Requirements
Simulation Block Diagram
Design Requirements
Functional Block Diagram
Analog input
RCM 3400
4 to 1
Analo
g
Mux
Digital control line
Ch A
Ch B
Ch C
Ch D
Digital
Prog
line
TI
MPS 430
OBC
Data
bus
I
2
C
Serial
bus
8 analog
line
IMU
Gyro
MAG
Attitude
Ephemerid
Design Overview
Design Overview
9V
Power Subsystem
Transceiver
Communications System
Sensor Payload
VREG
ADC
Microprocessor
Data Handling Unit
Humidity
5V & 3.3V Power
GPS
Temperature
Accelerometer
Wireless Camera
Antenna
Patch Antenna
Monopole Antenna
Light Intensity
•Thestructure&dimensions:
–Diameter:6.6cm
–Height:11.5cm
•Anyconstrainetc
•Specialneedordesign
•Structuralmaterials
•Toughnessetc
Body and Structure
Structure / Physical Design
Overall Structure
Structure / Physical Design
CRITICAL DESIGN REVIEW (CDR)
Electrical Power System
Electrical System Block Overview
Serial Terminal
Microprocessor
9V Power Supply Voltage Regulator
5V Power Supply
3.3V Power Supply
GPS
CMOS Camera
Sensor 1
Sensor 2
Sensor 3
Monopole Antenna
Ground Station
MMUSat
Sensors Testing: Preliminary Result
•Experiment on sensor for suitability of usage
0
5
10
15
20
25
30
35
06:05pm 06:35pm 07:05pm 07:35pm 08:05pm 08:35pm 09:05pm 09:35pm 10:05pm 10:35pm 11:05pm 11:35pm 12:05am 12:35pm 01:05am 01:35pm 02:05am 02:35pm 03:05am 03:35pm 04:05am 04:35pm 05:05am
Temperature (
o
C)
08082007 -EX1 Temperature Versus Time
Thermometer
Sensor1:
Temperature
Telemetry
Sensor2:
Temperature
Sensors Design Requirements
Sensors: Preliminary Result
•Sensor performance
•Suitability
•Sensor test procedures
Sensors Design Requirements
Sensors
Light intensity
Accelerometer
Temperature
Humidity
Microprocessor
Ground Base Station
Concept of Operation
Sensors Design Requirements
Each Sensor concept of operation
Concept of operation
Sensors Design Requirements
CRITICAL DESIGN REVIEW (CDR)
MMUSat: Weather Monitoring System
Data Handling Overview
Data Handling: uProc/uController
MMUSat: Weather Monitoring System
Microprocessor
•Themicroprocessorandspecs
•Whyitwaschosen
•Otheroptions???
Data Handling: Memory Budget
RCM 3400
Master
Bus
controlle
r
Memory
Allocation
(SRAM)
SPI
Serial
Bus
SLAVE
nIMU
&
Sensors
OBC MSP 430
Other
Peripherals,
(Sensors,
Actuator)
MASTER
RS232
Programming
Bus
Modem
I2C
SPI
Data Flow Block Diagram
Design Procedures
Integration and Test Overview
Integration and Test Overview
RCM 3400
Master
Bus
controlle
r
Memory
Allocation
(SRAM)
SPI
Serial
Bus
SLAVE
nIMU
&
Sensors
OBC MSP 430
Other
Peripherals,
(Sensors,
Actuator)
MASTER
RS232
Programming
Bus
Modem
I2C
SPI