Drone Autonomy Spec


I’ll create a structured takeover report covering both boards, architecture, completed work, current live state, known blockers, recovery history, verification gates, and the exact order a new engineer should follow.
Created a project doc

PCB Engineering Takeover Report

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PCB Engineering Takeover Report 1. Purpose and release status
This is the engineering handoff for the two-board KRYSTAL drone companion system. It consolidates the design intent, current implementation, known defects, routing history, verification evidence, and the recommended recovery sequence.
Current release status: HOLD — neither board is approved for fabrication or flight.
The next engineer should treat all counts in this report as the last confirmed state and rerun live ERC/DRC/layout checks before making changes. Do not generate Gerbers until every release gate in Section 13 passes.
2. Projects Safety / power / I/O base board
Created the comprehensive PCB Engineering Takeover Report.
It covers:
  • Both project links and board responsibilities
  • Current CM5 and S32K344 architecture
  • Power, camera, radar, autopilot, Wi‑Fi, FHSS and SIYI interfaces
  • Board dimensions, stackups and enclosure direction
  • Completed fixes and verified checks
  • Routing-service failure and recovery history
  • Known footprints, software and regulatory risks
  • Recommended takeover sequence
  • Fabrication-release gates
  • Immediate first-day checklist and required engineer deliverables
The report clearly marks both boards HOLD for fabrication until routing, interface freeze, DRC, thermal, software and mechanical validation are complete.
Review takeover report
Audit live board states
Prepare migration package
Freeze external interfaces

U4
U8
U3
J5
U2
U11
U7
J9
U1
J7
U6
J8
U9
R38
Resistance
1MΩ
R39
Resistance
31.6kΩ
R23
Resistance
10 Ω
R41
Resistance
681kΩ
R7
Resistance
33 kΩ
R10
Resistance
40.2 kΩ
R54
Resistance
31.6 kΩ
R5
Resistance
332 kΩ
R26
Resistance
100 kΩ
R48
Resistance
100 Ω
R6
Resistance
100 kΩ
R33
Resistance
4.02kΩ
R36
Resistance
10kΩ
R16
Resistance
20 kΩ
R2
Resistance
200 kΩ
R43
Resistance
10 kΩ
R40
Resistance
100kΩ
R4
Resistance
20.5 kΩ
R8
Resistance
100 kΩ
R44
Resistance
10 kΩ
R51
Resistance
10 kΩ
R29
Resistance
332 kΩ
R1
Resistance
1 kΩ
R13
Resistance
33 kΩ
R17
Resistance
10 kΩ
R30
Resistance
100 kΩ
R46
Resistance
68.1 kΩ
R31
Resistance
59 kΩ
R14
Resistance
33 kΩ
R9
Resistance
150 Ω
R34
Resistance
100kΩ
R45
Resistance
10 kΩ
R32
Resistance
100 kΩ
R53
Resistance
1 MΩ
R55
Resistance
681 kΩ
R28
Resistance
33 kΩ
R35
Resistance
10kΩ
R19
Resistance
1kΩ
R15
Resistance
698 kΩ
R21
Not Recommended for New Designs
Resistance
120Ω
R25
Resistance
316 kΩ
R12
Resistance
931 Ω
R52
Resistance
10 kΩ
R37
Resistance
22.1kΩ
R49
Resistance
1 kΩ
R47
Resistance
100 Ω
R27
Resistance
31.6 kΩ
R24
Resistance
10 Ω
R22
Resistance
120 Ω
R11
Resistance
5.6 kΩ
R50
Resistance
1 kΩ
R20
Not Recommended for New Designs
Resistance
120Ω
R18
Resistance
100 kΩ
R42
Resistance
12 kΩ
R3
Resistance
115 kΩ
R56
Resistance
100 kΩ
C12
Capacitance
2.2 uF
C41
Capacitance
100 nF
C17
Capacitance
10uF
C16
Capacitance
100nF
C19
Capacitance
100nF
C18
Capacitance
100nF
C33
Capacitance
10 uF
C40
Capacitance
100 nF
C21
Capacitance
100nF
C8
Capacitance
10 uF
C22
Capacitance
100 nF
C26
Capacitance
1 uF
C30
Capacitance
22uF
C38
Capacitance
1 uF
C3
Capacitance
10 uF
C11
Capacitance
2.2 uF
C6
Capacitance
2.2 nF
C37
Capacitance
100nF
C23
Capacitance
100 nF
C36
Capacitance
100nF
C5
Capacitance
22 uF
C39
Capacitance
47 uF
C1
Capacitance
2.2uF
C7
Capacitance
10 nF
C27
Capacitance
4.7uF
C4
Capacitance
4.7uF
C28
Capacitance
4.7uF
C34
Capacitance
1uF
C24
Capacitance
100 nF
C35
Capacitance
100uF
C13
Capacitance
100 pF
C10
Capacitance
2.2 uF
C32
Capacitance
100 nF
C9
Capacitance
10 uF
C2
Capacitance
0.22 uF
C15
Capacitance
100nF
C20
Capacitance
100nF
C29
Capacitance
2.2 nF
C14
Capacitance
22 pF
C31
Capacitance
10 uF
C25
Capacitance
100 nF
U10
U15
U17
MH4
D4
D5
U16
D3
U14
U13
J1
J6
L2
Inductance
22uH
J2
L1
Inductance
22 uH
J3
D7
D6
J4
D2
F1
U5
Q1
U12
D1
RF Regulatory Checklist — KRYSTAL Module
Singapore / IMDA Wi-Fi Requirement
The Singapore contract adds a dual-band Wi-Fi requirement:
  • IEEE 802.11ac/a/b/g/n
  • 2.412 GHz – 2.472 GHz and/or 5.15 GHz – 5.825 GHz
  • 2 dBi dual-band antenna
Candidate module under review: AP6256 dual-band 802.11ac Wi-Fi + Bluetooth module. Its datasheet indicates IEEE 802.11a/b/g/n/ac support, 2.4 GHz and 5 GHz operation, SDIO host interface, and small antenna reference of 0–2 dBi peak gain. Confirm Singapore IMDA approval path, allowed 5 GHz sub-bands, DFS/TPC obligations if applicable, and whether the exact module/antenna combination has acceptable modular approvals before production release.
SIYI A8 Mini Air Unit RF Review
The candidate SIYI A8 Mini payload includes an air unit specified by the customer as 5.100–5.825 GHz with a 5 dBi standard omni antenna. This must be handled as a separate RF emitter from KRYSTAL's onboard Wi‑Fi/LoRa design.
Regulatory actions:
  • Confirm the exact SIYI air-unit model, firmware region, rated TX power, modulation/bandwidth, and certification IDs.
  • Check Singapore/IMDA allowed 5 GHz sub-bands and whether DFS/TPC restrictions apply.
  • Confirm whether 5 dBi antenna gain is permitted with the air-unit TX power without exceeding EIRP limits.
  • Verify coexistence with KRYSTAL's planned dual-band Wi‑Fi, especially in 5 GHz operation.
  • Record whether the air unit is supplied as an already-approved subsystem or must be included in LOWALT's product approval package.
Customer-provided secondary safety radio:

Table


ItemValue
GCSRadioMaster TX16S Mark II 4IN1
ProtocolsFrSky / Spektrum family through internal 4IN1 module
Frequency band2.400–2.4835 GHz
EIRP<100 mW
Regulatory / integration actions:
  • Confirm Singapore/IMDA acceptance for the exact RadioMaster TX16S Mark II 4IN1 regional configuration.
  • Confirm the matching drone-side receiver model, antenna gain, protocol, and certification status.
  • Include the receiver/onboard radio, not only the GCS transmitter, in the full product RF coexistence plan.
  • Evaluate 2.4 GHz coexistence with KRYSTAL Wi‑Fi/Bluetooth and any SIYI or payload RF equipment.
  • Define failsafe behavior when the safety-radio link is lost, degraded, or overridden by autopilot logic.
Customer-provided tertiary data/video link:

Table


ItemValue
GCS / linkSIYI HM30 / MK32
Frequency band5.500–5.600 GHz required; verify exact device supports/locks to this range
Power<320 mW EIRP required
Architecture roleTertiary IP data/video link
Preliminary compatibility:
  • Architecturally suitable as an external data/video link because HM30/MK32-class systems provide Ethernet/IP and RTSP-style video workflows.
  • It is separate from KRYSTAL's onboard Wi‑Fi module and separate from the SIYI A8 Mini camera payload, though it may carry the A8 Mini's RTSP video.
Regulatory cautions:
  • Vendor material often lists 25 dBm / 320 mW transmit power; this may be conducted RF power, not EIRP. With antenna gain, EIRP can be higher than 320 mW.
  • Confirm exact antenna gain, region mode, firmware, conducted TX power, and certification IDs.
  • Check Singapore/IMDA authorization for 5.5–5.6 GHz operation, including any DFS/TPC/channel restrictions.
  • Confirm coexistence with KRYSTAL dual-band Wi‑Fi and any 5 GHz SIYI payload air unit.
Status
Draft — created when LoRaWAN capability was added to the schematic.
Wireless Technology Summary

Table


ModuleDesignatorTechnologyFrequency BandHost InterfaceNotes
Ezurio/Laird RM1262 / 453-00139RU6LoRaWAN / LoRa902–928 MHz RM1262; RM126x family also covers 863–870 MHz variantsUART with RTS/CTSModule uses MHF4 RF connector; final antenna, region SKU, and certification evidence must be locked before release.
Applicable Regulatory Tracks
  • FCC Part 15 / modular transmitter integration rules for US operation.
  • ISED for Canada if sold or operated there.
  • CE RED for EU operation; confirm correct 868 MHz regional variant and duty-cycle/channel-plan limits.
  • UKCA if sold in the UK.
RF Design Notes
  • Use the certified module integration guide and allowed antenna list for final antenna selection.
  • Keep the LoRa module antenna/RF connector at the board edge with copper keepout under/around the RF area per module datasheet.
  • Do not place high-current switching loops, Ethernet magnetics, or noisy clock traces near the LoRa antenna path.
  • The module RESETN pin is internally pulled to a 1.8 V domain and must not be driven directly by 3.3 V logic without level-compatible circuitry.
  • Region selection matters: 915 MHz for US-style operation, 868 MHz for EU-style operation.
Required Documentation Checklist
  • Wireless module identified in schematic: U6 453-00139R.
  • Confirm exact regional SKU and certification IDs.
  • Confirm antenna MPN and gain against module certification conditions.
  • Add antenna mechanical/RF keepout to PCB layout.
  • Confirm final LoRaWAN channel plan and transmit-power limits in firmware.
  • Export final schematic, BOM, PCB layout, and test reports before certification submission.
Open Items
  • Final antenna and enclosure are not selected.
  • Ethernet and compute-board architecture are provisional.
  • S32K344 pin mux for LoRa UART and expansion buses must be verified against the NXP IOMUX/reference manual.
  • Singapore / IMDA Wi-Fi Requirement

  • SIYI A8 Mini Air Unit RF Review

  • Safety Radio / GCS Link RF Review

  • SIYI HM30 / MK32 Data & Video Link RF Review

  • Status

  • Wireless Technology Summary

  • Applicable Regulatory Tracks

  • RF Design Notes

  • Required Documentation Checklist

  • Open Items