power sources electronics unit – lecture 5

28
LSU 11/05/2013 Electronics 5 1 Power Sources Electronics Unit – Lecture 5 Bench power supply Photovoltaic cells, i.e., solar panel Thermoelectric generator Battery Power Budget

Upload: kirestin-pollard

Post on 31-Dec-2015

45 views

Category:

Documents


0 download

DESCRIPTION

Power Sources Electronics Unit – Lecture 5. Bench power supply Photovoltaic cells, i.e. , solar panel Thermoelectric generator Battery Power Budget. Bench Power Supply. Adjustable, regulated output voltage Often includes a current limiting feature - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 1

Power SourcesElectronics Unit – Lecture 5

Bench power supply

Photovoltaic cells, i.e., solar panel

Thermoelectric generator

Battery

Power Budget

Page 2: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 2

Bench Power Supply

Adjustable, regulated output voltage

Often includes a current limiting feature

Great for designing and prototype testing

Not for flight

Page 3: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 3

Bench Power Supply

Important specifications:

Voltage range - should be 0 V to ~12 to 15 V

Load current - should be a few hundred mA

Regulation - hold output with a few tenths of V

Current limiting - very desirable if adjustable

can protect circuits from accidental damage

Page 4: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 4

Photovoltaic panel

Potential flight power source

“Free” electricity while Sun shines

Size and weight concerns

Expense

Page 5: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 5

Photovoltaic panelPanels made up of an array of individual cells

Each cell produces about 0.5 volt potential

Cell current depends on surface area and illumination

In full sun expect perhaps 10 milliwatts per cm2

For 6 V at 100 mA (600 mW) 12 cells would be needed, each having surface area about 5 cm2

Must face the Sun - and payload is probably rotating

Multiple panels needed - unless auto pointing

Page 6: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 6

Photovoltaic panelCells are delicate and subject to breakage

Voltage output may vary - electronic regulation needed

Backup battery needed for cloudy intervals

Not the best choice for short duration student flights

Page 7: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 7

ATIC

Page 8: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 8

Thermoelectric GeneratorUses the Seebeck Effect to convert a temperature difference directly into an electric current

Needs a heat source - deep space missions use the heat of radioactively decaying plutonium

Probably not a good choice for a student project ☺

Page 9: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 9

Battery

Strictly, a battery is a combination of discrete cells

Best choice for short duration flights

Inexpensive

Reasonably lightweight

Variety of voltages and energy capacities available

Page 10: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 10

Battery TypesPrimary batteries - one time use

carbon-zinc (old fashioned flashlight batteries)

alkaline (most common in consumer products)

silver-mercury (used in hearing aids and older cameras)

lithium - lots of energy for small weight

Rechargeable batteries - multiple charges/dischargeslead-acid (car batteries, or “gel cells”)

nickel-cadmium, Ni-Cd (older style rechargeable chemistry)

nickel-metal hydride, NiMH (popular now in consumer products)

lithium ion, (high end uses - laptop computers, digital cameras)

Page 11: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 11

Battery Characteristics

Terminal voltage - depends on specific chemistry

Capacity - rated in ampere-hours, or milliampere-hours3600*(ampere-hours)*(average terminal voltage) = energy capacity in joules

Physical size and weight - energy density in joule/gram

Discharge characteristics - especially at low temperature

Page 12: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 12

Battery Characteristics

Terminal voltage - depends on specific chemistry

carbon-zinc about 1.5 V per cell

alkaline - about 1.5 V per cell

lead acid - about 2.0 V per cell

Ni-Cd and NiMH - about 1.2 V per cell

lithium - about 1.5 V per cell

but often made as double-cells for 3 V

Page 13: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 13

Battery Characteristics

Capacity - rated in A-hr or mA-hr for small cells

Usually specified at the “ten-hour discharge rate”

Example - an Energizer AA 1.5 V lithium cell rated 2900 mA-hr

should deliver 290 mA for 10 hr before voltage falls below 1V

But, will not last proportionally as long at higher currents

Page 14: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 14

Battery CharacteristicsDischarge characteristics - the discharge curve

Use this typical lithium battery as an example

Nominal Voltage 3.0V

Rated Capacity 5Ah to 2.0V at 20°C (68 F)

Average Weight 55g (1.94oz)

Volume 26.5cm3 (1.60in.3)

Operating Temp. Range -20°C to 60°C (-4 F to 140 F)

Page 15: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 15

Battery Characteristics

Notice the degradation of capacity at low temperatures, especially at higher load currents.

And lithiums are about the best!

Page 16: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 16

Calculating a Power Budget

Given: minimum permissible voltage

maximum load current

average off-peak load current

load current versus time data (duty cycle)

mission duration

minimum expected temperature

Page 17: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 17

Power Budget Example

The GPS radio telemetry package:Transmitter requires a minimum supply voltage of 9 VGPS receiver requires from 3 V to 6 VFlight computer requires 5 V

If a single battery pack powers all three units, its terminal voltage cannot fall below 9 V.

Voltage regulators will be used to reduce the voltage for the other units.

Page 18: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 18

Power Budget Example

The GPS radio telemetry package:

GPS receiver draws 140 mA, continuously (100% duty)

Flight computer draws 50 mA, continuously (100% duty)

Transmitter draws 80 mA when in standby mode (93% duty)

Transmitter draws 1050 mA when transmitting (7% duty)(since transmitter sends a 2 second data burst every 30 seconds)

Peak current = 1320 mA, minimum current = 270 mA

Page 19: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 19

Power Budget ExampleThe GPS radio telemetry package:

GPS: 140 mA x 1 = 140 mA

Flight Computer: 0 mA x 1 = 50 mA

Radio Standby : 80 mA x 0.93 = 75 mA

Radio Transmit: 1050 mA x 0.07 = 74 mA

Add them up….. about 340 mA

If the beacon must operate for at least 8 hours…

340 mA x 8 hours = 2720 mA-hr required from the battery pack

Page 20: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 20

Power Budget Example

The GPS radio telemetry package:

A sufficient number of cells must be wired in series so that, even when delivering 1320 mA, the composite terminal voltage remains above 9 V, even at the minimum expected temperature.

Consulting the battery curves previously viewed, cell voltage can drop to about 2.2 V at -20 celsius when delivering 600 mA or more. Therefore, four cells will be needed. Allowing a reserve, cells should have a capacity of about 3000 mA-hr.

Page 21: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 21

Power Budget Example

Mission Duration Considerations

A science package must operate through pre-launch preparation and for the full duration of flight. If data is in non-volatile storage, it need not operate after touchdown. (~ 4 hours)

A tracking beacon must operate through pre-launch, the entire flight interval, and be able to continue well after touchdown to assure recovery. (8 hours or more)

Page 22: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 22

Voltage Regulator IC

Fixed Voltage outputs available (3.3, 5, 9, 12, 15, etc.) Vout < Vin -

Voh Positive or Negative models available

(Check pinout!) Variable Voltage models – set with

resistor values. LM317 Low Dropout models have lower

overhead voltage Ratings: Voltage In/Out, Max Current

Page 23: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 23

DC/DC Converter

Step-Up or Step-Down Voltage (or both) Uni-Polar, Bi-polar, or multiple Vout Specifications:

Voltage In (Min and Max) Voltage(s) Out Maximum Current, Maximum Power Out Efficiency: Pout = Pin*Efficiency

Mechanical (and Thermal) Packaging, connections Size and Weight

Page 24: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 24

Power System Example

Page 25: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 25

RegulatorsDC/DC Converters

Page 26: Power Sources Electronics Unit – Lecture 5

LSU 11/05/2013 Electronics 5 26

RegulatorsDC-DC Converters

12V50 mA

75 mA

20 mA

50mA

75mA

24V*20mA = 480mW

480mW/0.80= 600mW

I=P/V so I=600mW/12V

I = 50 mA if efficiency = 80%

I total= 50mA+75mA+50mA=175mA

Page 27: Power Sources Electronics Unit – Lecture 5

LSU 06/04/2007 Electronics 6 27

HOBO® Data Logger

Combines sensors, transducers, signal conditioning, A/D conversion, storage, and readout into a compact, battery powered unit.

Page 28: Power Sources Electronics Unit – Lecture 5

LSU 06/04/2007 Electronics 6 28

DIY Data Logger

Sketch a System Diagram for a data logger that logs a timestamp, temperature and battery voltages of two different packs (to compare alkaline and lithium battery performance.)