Picorover Design

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System Design
How Picorover system is defined
Date: 2009-Apr-23
Revision: 2.0
Prepared by: Joshua Tristancho
Revised by:
Date: 2009-Feb-13 Revision: 1.0 Prepared by: Joshua Tristancho Revised by: Andres Petilo
Date: 2009-Apr-23 Revision: 2.0 Prepared by: Joshua Tristancho Revised by:

Image:PicoroverZonalSubsystems_v1.0.JPG
edit functional committments

The system PicoRover is divided by three zones of functional commitments:

  • SHIELD FUNCTIONAL COMMITMENTS: A set of exposed subsystems.
  • CORE FUNCTIONAL COMMITMENTS: A set of critical subsystems in order to survive.
  • PAYLOAD FUNCTIONAL COMMITMENTS: A set of non critical subsystems but important for the mission.



Contents

Scientific Drivers

Principles and laws which make feasible to wing GLXP prizes with open access resources:

  1. Photoelectric effect: [1] Solar Cells.
  2. High power density batteries: [2].
  3. Thermoelectric effect:[3] Thermal feeding.
  4. Piezoelectric effect: [4] Micro force sensor.
  5. Electromagnetic induction effect: [5] Transformer.
  6. High integration level: [6] Embedded component.
  7. High density NAND memory:[7] Example of pendrive.
  8. Photodiode:[8] Example of HD camera.
  9. Accelerometer:[9] (IMU) Inertial Measurement Unit.
  10. Gyroscope:[10] Angular rate.
  11. Synthetic Aperture Radar: [11] Example of nano-SAR.

Edit Scientific Drivers

System schematics


Data flow

Data Flow Diagram

Image:PicoroverDataFlow_v1.2.JPG

Selected Components and Bandwidth

Image:PicoroverDataFlowBandwidth_v1.0.JPG

Picorover Parameters

Image:PicoroverParameters_v1.0.JPG

Picorover External Parameters

Parameter Type Bits Range Unit Nominal Bandwidth
Thermal Feeding Voltage float 32 0 to 5,000.0 Volts 0 V
(To be defined)
0.1 Hz
Radar Distance Density float array 2x100x32 0 to 30
0.1 to 10.0
meters
kilograms/cubic decimeter
0 m
1.200 kg/dm3
0.1 Hz
Foot Print Force float array 10x32 0 to 4,500.0 grams 0.0 g 40 Hz
External Temperature float 32 73 to 473
(-200 to +200)
Kelvin
(degree Celsius)
398K
(125 ºC)
0.1 Hz
HD Camera Streaming ? ? ? ? ?
Radio Link Ranging float 32 0 to 100,000.0 meters 0.0 m 0.1 Hz
Horizont Angle float 32 0 to 6.238185
(0 to 360º)
radians
(degrees)
0 rad
(0º)
1 Hz

edit external parameters

Picorover Internal Parameters

Parameter Type Bits Range Unit Nominal Bandwidth
Solar Feeding Voltage float 32 0 to 4.000 Volts 2.731 V 1 Hz
Battery Voltage float 32 0 to 4.000 Volts 3.300 V 1 Hz
Emergency Battery Voltage float 32 0 to 4.000 Volts 3.000 V 1 Hz
Chassis Temperature float 32 218 to 488
(-55 to +125)
Kelvins
(degree Celsius)
298K
(25 ºC)
1 Hz
Free Memory long 64 0 to 9,223,372,036,854,775,807 bytes 4 Gb 1 Hz
Local Time double 64 ±5.0E−324 to ±1.7E308 seconds Refered to the
launch moment
1000 Hz
Core to Shield Angle float 32 0 to 6.238185
(0 to 360)
radians
(degrees)
0 rad
(0 º)
40 Hz
Body Acceleration float array 3x32 -10 to +10
(-98.1 to 98.1)
Earth gravities
(meters/square second)
0.17 g
(1.6677 m/s2)
60 Hz
Body Angular Rate
Main motor rpm [1]
float array 3x32 0 to 6.981317
(0 to 400)
radians/second
(degrees/second)
0 rad/s
(0 º/s)
40 Hz
Target Pitch Angle float 32 0 to 6.238185
(0 to 360)
radians/second
(degrees/second)
0 rad/s
(0 º/s)
40 Hz
Target Roll Angle float 32 0 to 6.238185
(0 to 360)
radians/second
(degrees/second)
0 rad/s
(0 º/s)
40 Hz
Current Mode int32 32 (To be defined) DEFAULT 40 Hz
Labeling Illumination Boolean 32 0 or 1 FALSE 40 Hz

edit internal parameters

  1. Conversion factor to be specified

Subsystem List

SHIELD Subsystem Component list Weight Cost
Power Accumulating 2 Light weight capacitors 2 $2.00
Thermal Feeding 2 Thermoelectric cells 20 $70.00
Shield Transferring Not applicable for
Picorover1.3degrees
0 $0.00
Shield Heating 1 Thermoelectric cell 10 $35.00
Terrain Scanning 1 PicoSAR 10 $3,000.00
Terrain Feeling 12 Micro force sensors 12 $1,404.00
SUBTOTAL 54.00 grams $4,511.00
CORE Subsystem Component list Weight Cost
Solar Feeding 4 Solar cells 0.23 $10.00
Power Storing 2 Lithium Ion batteries 140 $20.00
Emergency Power Source 10 LiPo coin batteries 105 $50.00
Core Transferring Not applicable for
Picorover1.3degrees
0 $0.00
Core Heating 1 Thermoelectric cell 10 $35.00
Temperature Sensing 1 Temperature sensor 0 $0.00
Data Storing 1 USB pendrive
1 Host USB Controller
2.65 $35.00
Aligning Not applicable for
Picorover1.3degrees
0 $0.00
Processing 1 MCU Microcontroller 1 $50.00
Referencing 1 IMU Inertial Measurement Unit]]
To be replaced by a non-ITAR
sensitive component
7 $670.00
Attitude Controlling 1 Attitude Stepper Motor
1 MCU Microcontroller
1 IMU Inertial Measurement Unit
0
included in Processing
and Referencing
$200.00
Mission Managing 1 MCU Microcontroller 0
included in Processing
$0.00
Thrust Controlling 1 Thrust Stepper Motor
1 MCU Microcontroller
1 IMU Inertial Measurement Unit
0
included in Processing
and Referencing
$0.00
Shielding 1 Lead Shield 133.12 $1.00
SUBTOTAL 399.00 grams $1071.00
PAYLOAD Subsystem Component list Weight Cost
Downlink Transferring 1 Transceiver 1.28 $22.71
Recording 1 HD Camera
1 Cleared window
145
5.0
$2,000
$7.10
Labeling 1 GLXP label
1 White LED
0 $0.00
Ranging 1 Processor 0
included in
Downlink Transferring
$0.00
Uplink Transferring 1 Transceiver 0
included in
Downlink Transferring
$0.00
SUBTOTAL 151.28 grams $2,029.81
TOTAL 604.28 grams $7,611.81

edit subsystem list

Component List

353 HD Camera
Blueprint 353
ANR26650 Lithium Ion Battery
APR18650 Lithium Ion Battery
C8051F340 MCU Main Control Unit
To be replaced by Z430-RF2500
CL12 Light weight capacitor
CR2477 Lithium Coin Battery
DCBT-24AX Transceiver
To be replaced by Z430-RF2500
FR2505S Cleared window
Blueprint FR2505S
G1-1.0-127-1.27 Thermoelectric Cell
Blueprint G1-1.0-127-1.27
HT201-H Micro force sensor
KU204G USB Pendrive
ONI-23503-300-10-80 IMU Inertial Measurement Unit
To be replaced by ???
PL15S-020 Attitude Stepper Motor
Blueprint PL15S-020
T002A Thrust Stepper Motor Blueprint T002A
TASC27 Solar cell
VDIP2 MCU-USB Host
VNC1L Host USB Crontroller
To be replaced by VDIP2
XR-E White LED
Z430-RF2500 MCU Transceiver
Blueprint Z430-RF2500

edit component list

Part Tree

In progress

Picorover
SHIELD SUBSYSTEM
Subsystem Component list Size Drawing
Power Accumulating 2 Light weight capacitors
Thermal Feeding 2 Thermoelectric cell 34x31x3.2 mm
G1-1.0-127-1.27
Shield Transferring Not applicable for Picorover1.3degrees
Shield Heating 1 Resistor
Terrain Scanning 1 PicoSAR
Terrain Feeling 12 Micro force sensors

edit part tree shield subsystem

CORE SUBSYSTEM
Subsystem Component list Size Drawing
Solar Feeding 4 Solar cells
Power Storing 2 Lithium Ion batteries
Emergency Power Source 10 LiPo coin batteries
Core Transferring Not applicable for Picorover1.3degrees
Core Heating 1 Thermoelectric cell
Temperature Sensing 1 Temperature sensor
To be replaced by Z430-RF2500
32x20x2 mm
Z430-RF2500
Data Storing 1 USB pendrive
-
1 Host USB Controller
To be replaced by VDIP2
61x23x8 mm
14.2 grams
34x12x2 mm
1.7 grams
Aligning 3 Sensors 44x29x13 mm
D17.9 mm
-
T002A 94V-0
Processing 1 MCU Microcontroller
To be replaced by Z430-RF2500
32x20x2 mm
1.8 grams
Z430-RF2500
Referencing 1 IMU Inertial Measurement Unit
Attitude Controlling 1 Attitude Stepper Motor 67x15x15 mm
D15x10.5 mm
15.4 grams
PL15S-020
Mission Managing
Thrust Controlling 44x29x13 mm
D17.9 mm
19.4 grams
T002A 94V-0
Shielding D85/D76/D64x26 mm
60.9 grams
Window D54 mm
Bearing D45 mm
Al 0.1 mm

edit part tree core subsystem

PAYLOAD SUBSYSTEM
Subsystem Component list Size Drawing
Downlink Transferring 1 Transceiver 32x20x2 mm
Z430-RF2500
Recording 1 HD Camera

1 Cleared window
Elphel Camera
43.5x40.5x136.052 mm
Computar Lens
D41.6x48.8 mm
Window
D71.355x15 mm sphere96
Elphel 353


FR2505S
Labeling 1 GLXP label
1 White LED
GLXP label
Ranging 1 Transceiver 32x20x2 mm
Z430-RF2500
Uplink Transferring 1 Transceiver 32x20x2 mm
Z430-RF2500

edit part tree payload subsystem



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