Chapter 13: Spacecraft Subsystems Flashcards

1
Q

What is an EPS?

A

electrical power system that converts energy into usable electrical power to run the spacecraft

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2
Q

charge

A

q = 1.6E-19 Coulombs

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3
Q

current

A

i = dq/dt amps (C/s)

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4
Q

volts

A

v = PE/q volts (J/C)

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5
Q

resistance

A

R = v/i ohms (J*s/C^2)

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6
Q

power

A

P = iv watts (J/s)

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7
Q

What does the power supply do?

A

collects and converts energy and regulates power output

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8
Q

What does the power condition and distribution do?

A

adjusts voltages to match subsystem designs

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9
Q

What are common energy sources?

A
  1. solar (photo electric effect)
  2. chemical (electrolytes, anodes, cathodes)
  3. nuclear (heat from decaying isotopes)
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10
Q

Explain solar cell power

A

P=iv
peak power = Pmp
open circuit voltage = Voc
short circuit current = Isc

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11
Q

What is current density?

A

J=I/A_cell

used instead of I

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12
Q

What is the fill factor equation?

A

FF = VmpImp / VocIsc

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13
Q

The efficiency of power is?

A

η = Pout/Pin

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14
Q

What is the sun angle effect equation?

A

Pout = Pinηcos

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15
Q

What are some sources of chemical energy?

A

Li ion batteries
Nicad
NiH2

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16
Q

How are battery capacities rated?

A

rated against a particular discharge rate

17
Q

What are voltages based on?

A

based on current capacity (looses capacity over time)

18
Q

What in the hell is a Radioisotope Thermoelectric Generator?

A

generates voltage when radioactive decay of plutonium or uranium produces heat

19
Q

What is ADCS

A

attitude determination control system

keeps the spacecraft accurately and precisely pointed in the right direction

20
Q

What reference frame is used when determining location of a spacecraft?

A

the ECI or Earth centered inertial frame

21
Q

What reference frame is used when determining attitude of a spacecraft?

A

LVLH/ORB
local vertical, local horizon / orbiting frame
z axis towards center of earth (yaw)
y axis perpendicular to orbital plane (pitch)
x axis tangent to orbital plane (roll)

22
Q

What is the control system layout?

A
  1. sensors (where I am)
  2. desired attitude (where do I want to be)
  3. controller (how do I get there)
  4. actuators (apply the correction)
  5. dynamics (physics happen, bitch!)
23
Q

List the types of sensors

A
horizon/earth
sun sensor
star tracker
magnetometer
gyros
GPS
accelerometer
24
Q

What are some common actuators?

A

magnetorquers
reaction wheel
control movement gyros
thrusters

25
What are some environmental disturbances?
solar radiation pressure atmospheric drag gravity gradient magnetic field torque
26
What are some passive stablizers
gravity gradient spin stabilizer dampers
27
Determination
how well you know where your pointing
28
Control
how well you can point in the right direction and get there
29
What is the ADCS composed of?
sensors, actuators, attitude control software algorithms