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Peter
fc308c6507
conclusions, section in lit review on avionics systems/existing emulation systems, experimental results comparison
34 lines
8.0 KiB
Plaintext
34 lines
8.0 KiB
Plaintext
{"rule":"ABLE_TO_PASSIVE","sentence":"^\\QAs shown in figures \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q and \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q, the *g*-levels and bandwidth are relatively low and are able to be met by the LSM6DSO.\\E$"}
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{"rule":"UPPERCASE_SENTENCE_START","sentence":"^\\Qft y\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\QThere are multiple satellite qualification standards, an example is the NASA General Environmental Verification Specification (GEVS) which is a panel of tests including electromagnetic compatibility (EMC), thermal, acoustic and vibration tests that are required for all NASA Goddard Space Flight Center projects \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q.\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\QHonours Deliverables 2024-3-7 2024-10-18 Research proposal 2024-3-7 2024-04-19 Research proposal draft 2024-3-7 2024-4-16 Edit 2024-4-16 2024-4-19 [name=propwriting]Proposal Due 2024-04-19\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\QThesis 2024-4-19 2024-10-18 [name=startthesis]Record results, sketch out parts of thesis 2024-04-19 2024-08-07 Write thesis draft 2024-07-21 2024-09-24 [name=feedback]Get feedback, edit second draft 2024-09-25 2024-10-10 Final editing and typesetting 2024-10-10 2024-10-18 Thesis 2024-10-18\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\Q[link bulge=4]propwriting startthesis [link bulge=4]suborbital feedback\\E$"}
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{"rule":"UPPERCASE_SENTENCE_START","sentence":"^\\Qyear, month=shortname [title height=1.8, title label node/.append style=rotate=90]week [title/.style=opacity=0] 364\\E$"}
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{"rule":"COMMA_PARENTHESIS_WHITESPACE","sentence":"^\\QA HPR has a higher total impulse than model rockets but a lower impulse than sounding rockets, with a range of 36 up to 163840 , and have a sub-orbital trajectory unlike commercial launch vehicles \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q.\\E$"}
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{"rule":"A_INFINITIVE","sentence":"^\\QA Raspberry Pi Zero W is used for the OBDH system instead of an eMMC module and STM32L476 since: It reduces the cost of the PCB as the assembly of BGA packages such as eMMC adds significant cost per board, The Pi Zero W runs an operating system unlike the STM32, which simplifies development and debugging, The write speed of the Pi is larger than the STM32 and eMMC combination.\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\Qft y g bd\\E$"}
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{"rule":"UPPERCASE_SENTENCE_START","sentence":"^\\Qft y g bd\\E$"}
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{"rule":"UPPERCASE_SENTENCE_START","sentence":"^\\Qcircuit.js.\\E$"}
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{"rule":"A_INFINITIVE","sentence":"^\\QA Raspberry Pi Zero W is used for the OBDH system instead of an eMMC module and STM32L476 since: It reduces the cost of the PCB as the assembly of BGA packages such as eMMC adds significant cost per board, The Pi Zero W runs an operating system and can be controlled remotely from a PC unlike the STM32, which simplifies development and debugging, The write speed of the Pi is larger than the STM32 and eMMC combination.\\E$"}
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{"rule":"COMMA_PARENTHESIS_WHITESPACE","sentence":"^\\QAs shown in \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q the rocket reaches an apogee of 413 at 9.74 and the total flight time is 30 .\\E$"}
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{"rule":"COMMA_PARENTHESIS_WHITESPACE","sentence":"^\\QThe launch phase lasts only 1.6 and has a high average acceleration of 5.77 , as shown in \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q.\\E$"}
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{"rule":"POSSESSIVE_APOSTROPHE","sentence":"^\\QThe use of the FHSS allows the RFD900x to transmit at the maximum power of 1 that is allowable by the class license under the frequency hopping transmitters section \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q.\\E$"}
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{"rule":"COMMA_PARENTHESIS_WHITESPACE","sentence":"^\\QThe modem also contains a temperature range of -40 85 , which satisfies the range of temperatures required to pass the temperature testing.\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\QThe DAQ system must be able to track the HPR throughout the full launch to enable recovery as stated in section sec:hpr-test-req.\\E$"}
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{"rule":"ENGLISH_WORD_REPEAT_BEGINNING_RULE","sentence":"^\\QAfter soldering, the manual solder joints are inspected to ensure they are not cold joints, and the boards are again tested for short-circuits.\\E$"}
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{"rule":"UPPERCASE_SENTENCE_START","sentence":"^\\Qft y g axis bd mm DA oct\\E$"}
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{"rule":"MORFOLOGIK_RULE_EN_AU","sentence":"^\\QInitialise the LSM6DSOX by issuing the following commands: Ensure the WHOAMI register matches the expected value, Software reset the device, Wait for the device to be reset, Disable the I3C interface, Enable block data update, Set the scale for the accelerometer to 16 , the maxmium full scale possible, Set the sampling rate to 6666 and the batching rate to 12.5 , Set the FIFO to continuous mode (old samples are automatically discarded), Set FIFO watermark level to 384 samples, Set interrupt pin 1 to pulse on FIFO watermark being reached (this results in a pulse being generated on the INT1 pin when a large amount of data is present in the FIFO to be read, resulting in the interrupt handler being triggered.),\\E$"}
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{"rule":"ENGLISH_WORD_REPEAT_BEGINNING_RULE","sentence":"^\\QComponents will not be sourced from other suppliers for reasons including high minimum order quantities or counterfeit components.\\E$"}
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{"rule":"CD_NN","sentence":"^\\QThree 18650 cells were selected since this is the maximum number of cells which can fit on a 80 x 80 PCB using a 3 cell 18650 holder.\\E$"}
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{"rule":"COMMA_PARENTHESIS_WHITESPACE","sentence":"^\\QTwo 1 TP4056 linear battery chargers were connected in parallel to the battery pack to allow a maximum charging current of 2 .\\E$"}
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{"rule":"WHITESPACE_RULE","sentence":"^\\Qft y g axis bd mm DA oct\\E$"}
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{"rule":"BEEN_PART_AGREEMENT","sentence":"^\\QName Description HL constraints Stable in vacuum The DAQ system will be vacuum tested, therefore the cells need to be stable under vacuum P1 Wide temperature range Batteries must survive temperature testing Low cost Due to limited budget, space qualified batteries would be cost prohibitive High energy density and specific energy The system needs to support the payload for at least \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q at the worst-case power budget without recharging Reasonable power density and specific power The overall system needs to be able to provide at least \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q of current in a small space/mass, so the batteries should have similar current capacities.\\E$"}
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{"rule":"PHRASE_REPETITION","sentence":"^\\QTODO: Locking connectors Locking connectors must be used between the payload and DAQ due to the high vibration environment.\\E$"}
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{"rule":"PHRASE_REPETITION","sentence":"^\\QLongitudinal Lateral Sweep Rate Axis 1-4 Frequency Level Frequency Level \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q Three axes \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q Three axes Vibration Data: Longitudinal and Lateral Details with Sweep Rate and Axis Merged\\E$"}
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{"rule":"POSSESSIVE_APOSTROPHE","sentence":"^\\QThe use of the FHSS allows the RFD900x to transmit at the maximum power of \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q that is allowable by the class license under the frequency hopping transmitters section \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q.\\E$"}
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{"rule":"CD_NN","sentence":"^\\QThree 18650 cells were selected since this is the maximum number of cells which can fit on a \\E(?:Dummy|Ina|Jimmy-)[0-9]+\\Q PCB using a 3 cell 18650 battery holder.\\E$"}
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{"rule":"A_INFINITIVE","sentence":"^\\QThere was issues using the 4-bit mode on the eMMC, which limited the write and read speeds.\\E$"}
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{"rule":"LIGATURES","sentence":"^\\QThe shaker table tests were performed at AVI on the 2024-09-25 using a Brüel & Kjær LDS V8800 electrodynamic shaker table.\\E$"}
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{"rule":"LIGATURES","sentence":"^\\QA Brüel & Kjær type 4533-B integrated electronics piezoelectric (IEPE) accelerometer was used as the control and data accelerometer, which were mounted to the shaker table and the payload respectively.\\E$"}
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