morehead state university morehead, ky prof. bob twiggs rjtwiggs@gmail

Post on 01-Jan-2016

28 Views

Category:

Documents

0 Downloads

Preview:

Click to see full reader

DESCRIPTION

Power Systems Design - 1. Morehead State University Morehead, KY Prof. Bob Twiggs RJTwiggs@gmail.com. Power Systems Design - 1. Power System Design Considerations. System Requirements. Sources. Storage. Distribution. Control. 2. SSE -122. Power Systems Design - 1. 3. SSE -122. - PowerPoint PPT Presentation

TRANSCRIPT

Morehead State UniversityMorehead, KY

Prof. Bob TwiggsRJTwiggs@gmail.com

Power Systems Design - 1

1

2

Power System Design Considerations

Power Systems Design - 1

System Requirements

Sources

Storage

Distribution

Control

SSE -122

3

Power Systems Design - 1

SSE -122

4

Power Systems Design - 1

SSE -122

5

Operating regimes of spacecraft power sources

Power Systems Design - 1

SSE -122

6

Operating regimes of spacecraft power sources

Power Systems Design - 1

SSE -122

7

Power Systems Design - 1

SSE -122

8

Power Systems Design - 1

New Technology

SSE -122

9

Power Systems Design - 1

Sun spectral irradiance

Solar cell response

Peak sun irradiance

SSE -122

10

Power Systems Design - 1

SSE -122

11

Power Systems Design - 1

Dual Junction Cell

Added by second junction

Efficiency

SSE -122

12

Power Systems Design - 1

Use of the Sun’s Spectrum

SSE -122

13

Power Systems Design - 1

SSE -122

14

Power Systems Design - 1 Triple Junction Cell

Added by second junction

Added by third junction

Efficiency

SSE -122

15

Power Systems Design - 1

Reduce Efficiency

Good Efficiency

SSE -122

16

Power Systems Design - 1

SSE -122

17

Power Systems Design –I Ended 10/21/10

Max Cell Voltage when open circuit

Max Cell Current when short circuit

SSE -122

18

Power Systems Design - 1

Peak Power

SSE -122

19

Power Systems Design - 1

Add cell voltages to get string voltage

String of cells

Parallel strings to cover panel

Solar Cell Strings

SSE -122

20

Power Systems Design - 1

SSE -122

Power Systems Design - 1

ShadowingKills all power

SSE -122

22

Power Systems Design - 1

Some Solar Notes

SSE -122

23

Power Systems Design - 1

23

Sun

Approx Cosine

SSE -122

24

Power Systems Design - 1

Eclipse

Parallel Sun Rays

Sun

Earth

Satellite Orbit

SSE -122

Power Systems Design - 1

25

Gravity Gradient Stabilized

Sun

SSE -122

26

Power Systems Design - 1

Passive Magnetic Stabilized

N

S

SNSN

S N

S NS

N

S

N

S

N

S

N

S

N

S

N

S

N

SN

SN

SN

Sun

SSE -122

27

Inertially StabilizedPower Systems Design - 1

Sun

SSE -122

28

Power Systems Design - 1

Questions?

SSE -122

Morehead State UniversityMorehead, KY

Prof. Bob TwiggsRJTwiggs@gmail.com

Power Systems Design - 2

29

30

Power System Design Considerations

Power Systems Design - 2

System Requirements

Sources

Storage

Distribution

Control

SSE -122

31

Power Systems Design - 2

SSE -122

32

Power Systems Design - 2

SSE -122

33

Power Systems Design - 2

Primary Secondary

SSE -122

34

Power Systems Design - 2

• Primary – non rechargeable batteries

• Secondary – rechargeable batteries

Electrical Power Battery Storage

SSE -122

35

Power Systems Design - 2

Energy Storage

Not Rechargeable

SSE -122

36

Power Systems Design - 2 Not Rechargeable

SSE -122

Not Rechargeable

37

Power Systems Design - 2 Not Rechargeable

Not Good

SSE -122

38

Power Systems Design - 2 Rechargeable

Old Technology

SSE -122

39

Power Systems Design - 2 Rechargeable

Old Technology

SSE -122

40

Power Systems Design - 2 Rechargeable

Old Technology

SSE -122

41

Power Systems Design - 2 Rechargeable

SSE -122

42

Power Systems Design - 2 Rechargeable

New Technology

SSE -122

43

Power Systems Design - 2

• Use of NiCd batteries required reconditioning

• Reconditioning not required for Li Ion batteries.

Reconditioning battery system

Close sw to crowbar battery

Close sw to crowbar second battery

SSE -122

44

Power Systems Design - 2

How much Battery Charge Left?

Charging causes heating

Discharging causes heating

SSE -122

45

Power Systems Design - 2 Batteries

Most common form of electrical storage for spacecraft

Battery terms:Ampere-hour capacity = total capacity of a battery (e.g. 40 A for

1 hr = 40 A-hrDepth of discharge (DOD) = percentage of battery capacity used in

discharge (75% DOD means 25% capacity remaining. DOD usually limited for long cycle life)Watt-hour capacity = stored energy of battery, equal to

A-hr capacity times average discharge voltage.Charge rate = rate at which battery can accept

charge (measured in A)Average discharge voltage = number of cells in series times

cell discharge voltage (1.25 v for

most commonly used cells)SSE -122

46

Power Systems Design - 2

Considerations for power calculations

We have a battery that has a power capacity of:

1000mA (1000mAHrs)@ 1.2vIt can supply 1000mA for 1 hour or 500mA for 2 hours or 250mA for 4 hours @ a voltage of 1.2 v.Power rating of 1000mA x 1.2 v = 1.2 watt hours

SSE -122

47

Power Systems Design - 2

Battery selection:

SSE -122

48

Power Systems Design - 2

Considerations for power calculations

Two batteries in series.

SSE -122

49

Power Systems Design - 2

Considerations for power calculations

Two batteries in parallel.

SSE -122

50

Power Systems Design - 2 Rechargeable

SSE -122

51

Power Systems Design - 2

Questions?

SSE -122

Morehead State UniversityMorehead, KY

Prof. Bob TwiggsRJTwiggs@gmail.com

Power Systems Design - 3

52SSE -122

53

Power System Design Considerations

Power Systems Design - 3

System Requirements

Sources

Storage

Distribution

Control

SSE -122

54

Power Systems Design - 3

SSE -122

55

Power Systems Design - 3

Power Systems Design - 3 or EPS

Solar Panels - source

Charge Control

Batteries

Voltage

Bus

Voltage

DC/DC

Voltage

DC/DC

Subsystem

Subsystem

SSE -122

56

Power Systems Design - 3

Radios

• Fixed voltage busses (5v, -5v, 7v, 3.3v, 12v, etc.)

• Quieter – generates less noise on voltage bus

SSE -122

57

Power Systems Design - 3

• DC/DC Converter/Regulators

• Regulate 2 Li Ion batteries - ~7.2v 5v

• “Buck Up” 1 Li Ion battery - ~3.6v 5v

Requires less circuitry, more efficient to regulate down

Requires more circuitry, less efficient to “buck up” voltage.

SSE -122

58

Power Systems Design - 3

Could be caused by arcing due to spacecraft charging

Failure in subsystem that causes a short

Feedback on voltage bus from some components

Multiple return paths for current to battery – don’t use grounded frame

Power cycling required to reset components that have latch up due to radiation

SSE -122

59

Power Systems Design - 3

SSE -122

60

Power Systems Design - 3

SSE -122

61

Power Systems Design - 3

62

Power Systems Design - 3

What type of solar panel system does it take to generate 47.5 watts peak and 27.8 watts average?

63

Power Systems Design - 3

64

Power Systems Design - 3

Questions?

Morehead State UniversityMorehead, KY

Prof. Bob TwiggsRJTwiggs@gmail.com

Power Systems Design - 4

65SSE-122

66

Power Systems Design - 4

Power Systems or EPS

SSE-122

67

Power Systems Design - 4

SSE-122

68

Power Systems Design - 4

Look at the parts of the EPS

SSE-122

69

Power Systems Design - 4

Take Solar Panel

SSE-122

70

Power Systems Design - 4

5.6.

1350

1350

SSE-122

71

Power Systems Design - 4

What do we need from the solar panel?

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

Lets go back and look at the solar cell.

SSE-122

72

Power Systems Design - 4

This dual junction cell

1. Has an efficiency of ~ 22%2. Open circuit voltage ~ 2.2v3. Size – 76 x 37 mm

Lets go back and look at the solar cell.

SSE-122

73

Power Systems Design - 4

This dual junction cell

1. Has an efficiency of ~ 22%2. Open circuit voltage ~ 2.2v3. Size – 76 x 37 mm

Solar cell has an I-V curve like this

SSE-122

74

Power Systems Design - 4

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

This dual junction cell

1. Has an efficiency of ~ 22%

2. Open circuit voltage ~ 2.2v

3. Size – 76 x 37 mm

Looked at the solar cell.

SSE-122

75

Power Systems Design - 4

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

Need to select a battery to design forsolar panel voltage

SSE-122

76

RechargeablePower Systems Design - 4

SSE-122

77

Power Systems Design - 4

Use a lithium ion batteryLi Ion batteries = 3.6 v nominal

Design Criteria for charging Li Ion battery:

1. Need 10-15% more voltage to charge than the nominal voltage.

2. Here we would need solar panel voltage of ~ 4.0 – 4.2v to charge this battery.

Design Criteria solar panel:

1. Number of cells = Max voltage/cell voltage.

2. Take minimum number of whole cells.

# cells = (4.2v/string)/(2.2v/cell) = 1.9 or 2 cell for a string voltage of 4.4v

SSE-122

78

Power Systems Design - 4

SSE-122

79

Power Systems Design - 4

Use two lithium ion batteriesLi Ion batteries = 7.2 v nominal

Design Criteria for charging Li Ion battery:

1. Need 10-15% more voltage to charge than the nominal voltage.

2. Here we would need solar panel voltage of ~ 8.0 – 8.3v to charge this battery.Design Criteria solar panel:

1. Number of cells = Max voltage/cell voltage.

2. Take minimum number of whole cells.

# cells = (8.3v/string)/(2.2v/cell) = 3.77 or 4 cell for a string voltage of 8.8v

Lets be conservative and use 5 cells for 11v.

SSE-122

80

Power Systems Design - 4

Now we have:

Two Li Ion batteries = 7.2 v nominal

5 cells for 11v to charge with.

SSE-122

81

Power Systems Design - 4

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

What is packing factor?

Got

Got

SSE-122

Total Panel Area

82

Power Systems Design - 4

Packing Factor

Packing Factor = Total Cell Area/ Total Panel Area

Total Cell Area

SSE-122

83

Packing Factor

What do you do if given a fixed size panel on which to put solar cells and you have these different size solar cells?

Fixed solar panel size

Cell type 3

Cell type 1 Cell type

2

Power Systems Design - 4

SSE-122

84

Packing Factor

What do you do if given a fixed size panel on which to put solar cells and you have these different size solar cells?

Power Systems Design - 4

SSE-122

85

Power Systems Design - 4

Now we have:5 cells for 11v where the string has all of the cells hooked in series

11v

Total Panel Area

How do you mount these 5 cells on this panel?

SSE-122

86

Power Systems Design - 4

How do you mount these 5 cells on this panel?

NO!OK!

Visually we can see a very poor packing factor.

SSE-122

87

Power Systems Design - 4

What if the cells were bigger?

Oh Oh!

Now you have only 4.4v in the string.

SSE-122

88

Power Systems Design - 4

Can’t do. All cells for a single string must be on same face.

Got a cube? Put other cells on another face?

SSE-122

89

Power Systems Design - 4

Where are we now in the solar panel design?

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

Assume we could mount the 5 cells on a panel, what is total power for the cells selected?

Got

Got

Not got, but understand

SSE-122

90

Power Systems Design - 4

How much power from these cells?5 cells for

11v

11v

One cell area = 76 x 37 mm = 2812 mm^2Total cell area = 8*2812 = 22496 mm^2 = 2.25 x10-2 m^2

We have 1350 watts/m^2 from the sun in space

Direct power = (1350 w/m^2) x (2.25 x10-2 m^2) = 34.4 watts

Converted power = direct power x cell efficiency = 34.4 w x 0.22 eff

= 7.5 watts7.5 wattsFor this dual junction cell

1. Has an efficiency of ~ 22%

2. Open circuit voltage ~ 2.2v

3. Size – 76 x 37 mmSSE-122

91

Power Systems Design - 4

Where are we now in the solar panel design?

What are the attributes of a solar panel?

1. Total output power of solar panel.2. Voltage of solar panel.3. Maximum packing factor.4. Efficiency of the solar cells.5. Operating temperature of the panels.

Now we can assume to start:1. panel is at 90 degrees with sun – max power2. operating temperature 20 degrees.. Centigrade –

22% eff

Got

Got

Not got, but understand

Got

Don’t forget, temperature counts a lot.

SSE-122

92

Start here Tuesday for Idaho

Power Systems Design - 4

SSE-122

93

Power Systems Design - 4

Now that we have beat our way through the solar panel design ----- lets go look at the some more parts of the EPS.

SSE-122

94

Power Systems Design - 4

Power Systems or EPS

What is this?

SSE-122

95

Power Systems Design - 4

Power Systems or EPS

Back bias diode

When panel 1 is shaded, the back bias diode keeps the current from flowing backwards through panel 1, when panel 2 is generating a voltage across it.

Panel 1

Panel 2

SSE-122

96

Power Systems Design - 4

Power Systems or EPS

What is this?

R V

Measure current by measuring voltage across a low resistance precision resistor

SSE-122

97

Power Systems Design - 4Power Systems or EPS

SSE-122

98

Power Systems Design - 4Power Systems or EPS

SSE-122

99

Power Systems Design - 4

SSE-122

100

Power Systems Design - 4

SSE-122

101

Power Systems Design - 4Expanded subsystem control

SSE-122

102

Power Systems Design - 4Expanded subsystem control

SSE-122

103

Power Systems Design - 4

What does a charge regulator do?

1. Controls voltage from PV to battery2. Controls rate of charge3. Prevents overcharging4. Can “boost” or “buck” PV voltage to match

battery needs.

SSE-122

104

Power Systems Design - 4Expanded subsystem control

SSE-122

105

Power Systems Design - 4

Consider:

When high current occurs in a subsystem, it could be from latch-up. What to do? Cycle power. Where do you do this – hardware controlled in the EPS.

SSE-122

106

Power Systems Design - 4

Consider the satellite’s attitude control for solar power generation.

SSE-122

107

Eclipse

Parallel Sun Rays

Sun

Earth

Satellite Orbit

Power Systems Design - 4

SSE-122

108

Gravity Gradient StabilizedPower Systems Design - 4

SSE-122

109

Passive Magnetic Stabilized

N

S

SNSN

S N

S NS

N

S

N

S

N

S

N

S

N

S

N

S

N

SN

SN

SN

Power Systems Design - 4

SSE-122

110

Inertially StabilizedPower Systems Design - 4

SSE-122

111

Power Systems Design - 4

SSE-122

112

Power Systems Design - 4

SSE-122

113

• Power from sun in orbit ~ 1350 watts/meter2

• Power from cells on ground ~ 35% less than in space

• Can get some power form albedo – earth shine ~ 35%

Some Solar Notes

Power Systems Design - 4

SSE-122

114

Power Systems Design - 4

SSE-122

115

Power Systems Design - 4

Need to consider the power requirements of all of the subsystems and when they are used to build a power budget.

SSE-122

116

Power Systems Design - 4

Questions?

SSE-122

top related