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GNC quiz
Sample questions
Rules
• 3 rounds:
• Round 1: 13 x General – 2 points each
• Round 2: 8 x Anagrams- 1 point each
• Round 3: 2 x Connect questions- 4 points each
Identify X
“The Apollo computer used 2k
of magnetic core RAM and 36k
wire rope [...]. The CPU was built
from ICs [...]. Clock speed was
under 100 kHz [...]. The fact that
the MIT engineers were able to
pack such good software (one of
the very first applications of the
X filter) into such a tiny
computer is truly remarkable.”
— Interview with Jack Crenshaw,
Identify X
Rudolf Kalman (Kalman
filter)
https://en.wikipedia.org/
wiki/Rudolf_E._K%C3%A1
lm%C3%A1n
Identify mission
(where this guidance was used)
Chang’e 3
https://www.researchgate.net/publication/28434
5092_Guidance_Summary_and_Assessment_of_t
he_Chang'e-3_Powered_Descent_and_Landing
What are these called?
‘Feelers’
http://heroicrelics.org/info/lm/lunar-surface-
probe.html
What is being shown in the figure below?
Falcon 9 booster landings
Name and explain this effect,
Sagnac effect
• Relates the change in path length to change in wavelength due to a
rotation rate
Identify mission?
Arrived at Moon
May 30, 1966 landed on Oceanus Procellarum
September 20, 1966 crashed near Copernicus crater
April 17, 1967 landed on Oceanus Procellarum
July 14, 1967 crashed on Sinus Medii
September 8, 1967 landed on Mare Tranquillitatis
November 7, 1967 landed on Sinus Medii
January 7, 1968 landed near Tycho crater
Surveyor
Arrived at Moon
July 14, 1967 crashed on Sinus Medii
September 8, 1967 landed on Mare Tranquillitatis
November 7, 1967 landed on Sinus Medii
January 7, 1968 landed near Tycho crater
Identify X and Y
X, Y= Luna 9 and
Surveyor 1
Connect
• Academy of Science, Saint Petersburg
Lyapunov
https://en.wikipedia.org/wiki/Lyapunov_function
https://en.wikipedia.org/wiki/Aleksandr_Lyapunov
• Academy of Science, Saint Petersburg
Identify X
• It was determined that the chain of events that led to the spacecraft's loss began
with its X. The attitude control system attempted to use Hitomi's reaction
wheels to counteract the non-existent spin, which caused the spacecraft to rotate
in the opposite direction. Because the X continued to report faulty data, the
reaction wheels began to accumulate excessive momentum, tripping the
spacecraft's computer into taking the vehicle into "safe hold" mode. Attitude
control then tried to use its thrusters to stabilise the spacecraft; the sun
sensor was unable to lock on to the Sun's position, and continued thruster firings
caused Hitomi to rotate even faster due to an incorrect software setting. Because
of this excessive rotation rate, early on 26 March several parts of the spacecraft
broke away, likely including both solar arrays and the extended optical bench.
X=IRU/Gyro
• It was determined that the chain of events that led to the spacecraft's loss began
with its X. The attitude control system attempted to use Hitomi's reaction
wheels to counteract the non-existent spin, which caused the spacecraft to rotate
in the opposite direction. Because the X continued to report faulty data, the
reaction wheels began to accumulate excessive momentum, tripping the
spacecraft's computer into taking the vehicle into "safe hold" mode. Attitude
control then tried to use its thrusters to stabilise the spacecraft; the sun
sensor was unable to lock on to the Sun's position, and continued thruster firings
caused Hitomi to rotate even faster due to an incorrect software setting. Because
of this excessive rotation rate, early on 26 March several parts of the spacecraft
broke away, likely including both solar arrays and the extended optical bench.
• https://en.wikipedia.org/wiki/Hitomi_(satellite)
Connect
Attitude estimation using Kalman filter
https://arc.aiaa.org/doi/10.2514/3.56190
Markley, Schuster,Kalman Filter
What is happening here?
Hayabusa touchdown
Documentary:
https://www.youtube.com/watch?v=1GWsIzU-bm0
Identify X
On the basis of the outcome of the investigations performed, the SIB
members identified four main root causes that led to the X failure: -
1. Insufficient conservative modelling of the parachute dynamics
which led to expect much lower dynamics than observed in flight; -
2. Inadequate persistence time of the IMU saturation flag and
inadequate handling of IMU saturation by the GNC;
3. Insufficient approach to FDIR and design robustness;
4. Mishap in management of subcontractors and acceptance of
hardware, (the persistence of IMU saturation time was not
recorded at acceptance and instead believed to be 15 ms).
X: Schiaparelli
On the basis of the outcome of the investigations performed, the SIB
members identified four main root causes that led to the X failure: -
Insufficient conservative modelling of the parachute dynamics which led to
expect much lower dynamics than observed in flight; - Inadequate
persistence time of the IMU saturation flag and inadequate handling of IMU
saturation by the GNC; - Insufficient approach to FDIR and design robustness;
- Mishap in management of subcontractors and acceptance of hardware,
(the persistence of IMU saturation time was not recorded at acceptance and
instead believed to be 15 ms).
http://exploration.esa.int/science-e/www/object/doc.cfm?fobjectid=59175
What?
LM Powered-flight Attitude Control
Anagrams
Anagrams: 1 word
NadaAnarchy
Hint: Mission
Anagrams: 1 word
Chandrayaan
Hint: Mission
Anagrams: 1 word
Naga Layman
Hint: Mission
Anagrams: 1 word
Mangalyaan
Hint: Mission
Anagrams: 3 word
Advantaged Anointing Councilor
Hint:
Anagrams: 3 word
Guidance, Navigation and Control
Hint:
Anagrams: 3 words
Alan Refundment Tickles
Anagrams: 3 words
Unscented Kalman Filter
Anagrams: 3 words
Adele clouding scoop
Anagrams: 3 words
Closed loop guidance
Anagrams: 1 word
can soup
Anagrams: 1 word
Canopus
Anagrams: 4 word
announcer pile reshuffle
Hint: 60, 000 km
Anagrams: 4 word
Lunar sphere of influence
Hint: 60, 000 km
Anagrams: 1 word
• Rendezvous
Anagrams: 2 words
Garland Indra
Anagrams: 2 words
Landing radar
Connect
https://www.vanderbilt.edu/usli/2017/01/04/imu-mishaps-plague-recent-nasa-esa-missions/
Connect
StereoB, Schiaparelli, Hitomi
Recent missions suspected to fail due to gyro/IMU problems
https://www.vanderbilt.edu/usli/2017/01/04/imu-mishaps-plague-recent-nasa-esa-missions/
Connect
Connect
Moon Impact probe, Shackleton Crater, Minerology discovered by
Chandrayaan mission. Evidence of water-ice on the moon.

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Spacecraft Guidance, Navigation and Control Quiz