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Quadcopter Payload Delivery - PDR

Group 38:�Chuong Tran, Justin Quan, Dillon Kim, Brandon Hsi, Jaydon Schoonenberg, Alex Stefany

Week 6 - Fall 2025

Team 1

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Team Members

Sponsor: Mohamed Shorbagy

Team 2

Chuong Tran

4th Year�Mechanical and Aerospace Engineering

Alex Stefany�4th Year�Mechanical Engineering

Dillon Kim

4th Year�Mechanical Engineering

Brandon Hsi�4th Year�Mechanical and Aerospace Engineering

Jaydon

Schoonenberg

5th Year

Mechanical Engineering

Justin Quan

5th Year

Mechanical Engineering

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Contents

  1. Project Overview
  2. Review of PDP, Requirements, STnE
  3. Updated Structural Hierarchy
  4. Structural Decomposition & Management
  5. Equations
  6. Trade Studies
    1. Bubble Sorting Criteria
  7. CAD
  8. Timelines
  9. Fabrication Plans
  10. Technical Concerns and Conclusions

Chuong 3

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Project Overview

Chuong 4

Problem Definition:

Local businesses and pharmacies require autonomous deliveries to avoid ground traffic and save costs.

Patients that need quick delivery services like the elderly, disabled, and busy schedules would benefit from autonomous deliveries.

Design and operate an autonomous quadcopter capable of delivering a 1lb payload.

+

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ConOps (5W’s 1H)

Chuong 5

Questions:

Answers:

Who?

Businesses, pharmacies, non-abled patients, clients, operators, design engineers

What?

Pharmaceutical payloads, autonomy, flight control, deliveries

Where?

Congested urban metros

When?

Rush hours, daytime operations, perhaps 24/7

Why?

Aid in deliveries, cut delivery times, reduce effort, cost, and energy in physically retrieving packages.

How?

Autonomous UAV to deliver payloads over short-range deliveries.

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Requirements & STnE

Chuong 6

Constraint Requirements

  • C-1: The total system cost shall be less than $600
  • C-2: The components shall be mostly COTS parts, with exception to custom PCBs.
  • C-3: The design shall operate without the aid of a physical RC.

Functional Requirements

  • F-1: The quadcopter shall autonomously take off from a designated launch point.
  • F-2: The prototype shall navigate from the launch point to a target waypoint located 50 m away.
  • F-3: The quadcopter shall deliver the payload within 1 m of the target.
  • F-4: The quadcopter shall hover a minimum of 10 m above terrain.

Performance Requirements

  • P-1: The quadcopter shall stabilize its position within 5 seconds when stabilizing its position during the mission.
  • P-2: The payload release system shall deploy within 1 m of the targeted drop-off location.
  • P-3: The quadcopter shall cruise at an airspeed of 5 m/s at a minimum altitude of 10 m.

Quality-Attribute Requirements

  • QA-1: The quadcopter shall have protected electrical components from environmental factors
  • QA-2: The payload shall carry pharmaceutical items safely and properly (e.g. refrigeration, orientation, sealed)
  • QA-3: The quadcopter shall be operated safely in rural communities abiding by airspace codes.

Stakeholder Needs

ST-UN-001

Quadcopter shall safely deliver 1lb payloads to local pharmacies and businesses.

ST-UN-002

Quadcopter should operate autonomously without RC.

ST-UN-003

Quadcopter should avoid obstacles during deliveries.

ST-UN-004

Quadcopter’s total cost shall be less than $600.

ST-UN-005

Quadcopter shall be complying to airspace rules in any community.

ST-UN-006

Quadcopter should be rechargeable or maintainable.

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Structural Hierarchy

Jaydon/Alex 7

Quadcopter Delivery

Payload & Delivery Subsystem

Propulsion Subsystem

Chassis Subsystem

Controls Subsystem

Flight Controller

IMU

Magnetometer + Barometer

GPS

ESCs

Camera/LIDAR

Mission Planner + Telemetry

Payload Carrier

Release Mechanism

Landing Pad

Frame

Aeroshell

Electronic Mounts

Brushless Motors

Propellers

Batteries

Target Locator

Receiver

Major Components

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Structural Hierarchy (Individual Components)

Jaydon/Alex 8

Quadcopter Delivery

Payload & Delivery Subsystem

Propulsion Subsystem

Chassis Subsystem

Controls Subsystem

Flight Controller

(HolyBro Pixhawk 6C)

IMU

(HolyBro Pixhawk 6C)

Magnetometer + Barometer

(HolyBro Pixhawk 6C)

GPS

(M9N GPS)

ESC

(4x 20A ESCs)

Camera/LIDAR

(IMX219 Auto Focus Camera)

Mission Planner + Telemetry

(HGD-TELEM433)

Payload Carrier

(3D Printed)

Release Mechanism

(55g Metal Gear Torque Digital Servo Motor)

Landing Pad

(Provided)

Frame

(F450 Multi-Rotor QuadCopter Airframe)

Aeroshell

(3D Printed)

Electronic Mounts

(DJI F450 Quadcopter Board)

Brushless Motors

(Emax MT2213)

Propellers

(1045 Propellers)

Batteries

(4S LiPo)

Target Locator

(AruCo QR Code)

Receiver

(FS-iA6)

Power Distribution Board

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Structural Decomposition

Jaydon/Alex 9

Subsystem

Form

Function

Requirements

Chassis

(Alex & Justin)

Overall Form: Modular frame with integrated landing gear

Component 1: Main frame arms and central hub

Component 2: Aeroshell

Component 3: Mounting plates and vibration-isolating grommets

Function: Provide structural support and protection for all onboard systems

  • Subfunction 1: Support propulsion loads and distribute weight evenly�
  • Subfunction 2: Absorb vibration and impact during landing

R1.1 Minimum Factor of Safety Shall be Under operating loads Loads - Ideal 2.0 - Marginal 1.5

R1.2 - Chassis Ground Clearance Shall be - Ideal 20mm - Marginal 15mm

R1.3 Size Compliance with Government Regulations - Ideal Yes - Marginal Yes

Payload & Delivery

(Jaydon & Brandon)

Overall Form: Servo-actuated payload release mechanism with housing mount�

Component 1: Payload housing / bracket�

Component 2: Servo and Latch�

Component 3: Landing pad

Function: Secure, carry, and release payload accurately at target location

  • Subfunction 1: Retain payload during operation and various flight conditions�
  • Subfunction 2: Release payload autonomously upon GPS command

R2.1 Payload Release Accuracy Shall be- Ideal < 1m - Marginal <2m

R2.2 Release Deploy Time - Ideal < 1 s - Marginal <2s

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Structural Decomposition Cont.

Jaydon/Alex 10

Subsystem

Form

Function

Requirements

Controls

(Chuong)

Overall Form: Flight controller with onboard sensors and telemetry

Component 1: Pixhawk (or similar) flight controller

Component 2: GPS + IMU sensor

Component 3: Radio telemetry module

Function : Maintain stable, autonomous flight and navigation

  • Subfunction 1: Process sensor data for stabilization (PID control)�
  • Subfunction 2: Execute waypoint-based autonomous pathing

R3.1 Autonomous Target Accuracy Shall be - Ideal 1m - Marginal 2m

R3.2 No Physical RC Shall be Required - Ideal Yes - Marginal Yes

R3.3 Target Time for Mission Shall be- Ideal 45s - Marginal 60s

Propulsion

(Dillon)

Overall Form: Four-motor brushless propulsion system

Component 1: Brushless DC Motors

Component 2: Electronic Speed Controllers

Component 3: Propellers (10 in)

Function: Generate thrust for lift and maneuvering

  • Subfunction 1: Convert electrical power into mechanical thrust�
  • Subfunction 2: Adjust individual motor speeds for attitude control

R4.1 Cruise Speed Shall be - Ideal 5m/s, Marginal 3m/s

R4.2 Shall Maintain Altitude with Payload - Ideal > 10m - Marginal > 10m

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Preliminary Equations (Motor Spec)

Brandon 11

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Trade Studies - Frame

Brandon 12

Quadcopter Frame (Type) Weighted Matrix

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Lightweight*

25

3

0.75

4

1

4

1

2

0.5

Loading

20

4

0.8

4

0.8

4

0.8

5

1

Maintenance**

20

4

0.8

4

0.8

2

0.4

5

1

Durability

15

3

0.45

4

0.6

5

0.75

4

0.6

Simplicity

10

3

0.3

4

0.4

5

0.5

2

0.2

Manufacturing Cost***

5

4

0.2

4

0.2

2

0.1

2

0.1

Ease of Assembly

5

3

0.15

5

0.25

3

0.15

5

0.25

Sums

100

3.45

4.05

3.7

3.65

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Trade Study - Payload Mechanism

Jaydon/Justin 13

Quadcopter Payload Weighted Matrix

Sling Load (Rope + Crate)

REFERENCE

Grabber (Servo + Claw)

Integrated (Cage)

Drop Release

(Arm + Servo)

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Controllable*

25

3

0.75

4

1

5

1.25

5

1.25

Loading

20

3

0.6

3

0.6

5

1

4

0.8

Security

20

2

0.4

3

0.6

4

0.8

4

0.8

Durability

15

2

0.3

2

0.3

4

0.6

3

0.45

Simplicity

10

2

0.2

3

0.3

1

0.1

4

0.4

Manufacturing Cost**

5

2

0.1

3

0.15

1

0.05

2

0.1

Ease of Assembly

5

3

0.15

3

0.15

2

0.1

4

0.2

Sums

100

2.5

3.1

3.9

4

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Trade Study - Flight Controller

Dillon 14

Quadcopter Flight Controller Trade Study

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Programmability*

25

4

1

3

0.75

3

0.75

Ease of Autonomy**

20

5

1

3

0.6

1

0.2

Mass

20

3

0.6

3

0.6

4

0.8

Electronic Compatibility

15

4

0.6

3

0.45

3

0.45

Simplicity

10

3

0.3

3

0.3

4

0.4

Cost

5

1

0.05

4

0.2

3

0.15

Ease of Installation

5

3

0.15

4

0.2

5

0.25

Sums

100

3.7

3.1

3

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Trade Study - Propeller

Dillon 15

Quadcopter Propeller Weighted Matrix

Readytosky 6Pairs 1045 Propellers

1045 Propeller Pair Black

JMT 1045 CF propellers

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Thrust

30

3

0.9

4

1.2

2

0.6

Weight

20

4

0.8

3

0.6

2

0.4

Safety

20

3

0.6

2

0.4

3

0.6

Manufacturing Cost

20

4

0.8

3

0.6

4

0.8

Durability

10

4

0.4

2

0.2

3

0.3

Sums

100

3.5

3

2.7

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Trade Study - GPS

Dillon 16

Quadcopter GPS Weighted Matrix

HolyBro M10 GPS

HolyBro M9N GPS

HolyBro Micro M10

Holybro Micro M9

Holybro Micro M9

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Controllable

30

3

0.9

5

1.5

2

0.6

2

0.6

2

0.6

Accuracy

30

3

0.9

3

0.9

2

0.6

1

0.3

4

1.2

Size

20

2

0.4

3

0.6

2

0.4

2

0.4

4

0.8

Cost

20

2

0.4

4

0.8

4

0.8

3

0.6

3

0.6

Sums

100

2.6

3.8

2.4

1.9

3.2

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Trade Study - Motors

Dillon 17

Quadcopter Motors Weighted Matrix

XRotor FPV 2812 Motors

Readytosky 2212 920 KV brushless motors

Emax MT2213-935KV 2212

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Rating

Weighted Score

Controllable

25

3

0.75

4

1

5

1.25

Thrust

20

3

0.6

3

0.6

5

1

Weight

20

2

0.4

3

0.6

4

0.8

Safety

15

3

0.45

2

0.3

4

0.6

Manufacturing Cost

10

2

0.2

2

0.2

3

0.3

Ease of Assembly

10

2

0.2

2

0.2

3

0.3

Sums

100

2.6

2.9

4.25

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Trade Study - Battery

Justin 18

Quadcopter Battery Weighted Matrix

Spektrum 11.1V 5000mAh

CNHL RC Lipo Battery 4S

Criterion

Weight (%)

Rating

Weighted Score

Rating

Weighted Score

Battery Life

50

3

1.5

4

2

Size

25

3

0.75

4

1

Cost

25

4

1

3

0.75

Sums

100

3.25

3.75

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Bill of Materials

Justin 19

Item

QTY

Part Name

Part Number

Dimensions

Mass (g)

Unit Cost

Total Cost w/o Shipping

Total Cost w/ Shipping

1

1

Holybro Pixhawk 6C Mini (Model B)

02-0001

58.3 x 39 x 18.15mm

46.8

$129.00

$139.32

$148.23

2

1

F450 Quadcopter Frame

01-0001

363 x 363 x 40mm

282

$18.00

$19.44

$19.44

3

1

Drop Release Lock

03-0001

88 x 28 x 3.46 mm

35

$10.86

$11.73

$11.73

4

2

Deego MG996R Servo Motor

03-0002

47.6 x 53.6 x 20mm

55

$9.99

$10.79

$10.79

5

1

Flywoo GOKU G45M 45A 3-6S AM32 4-in-1 ESC - 20x20

01-0002

33 x 30 x 6.1mm

6.4

$51.99

$56.15

$63.15

6

4

Emax MT2213-935KV 2212

04-0001

27.9 x 39.7mm

55

$59.79

$64.57

$64.57

7

1

CNHL RC Lipo Battery 4S 14.8V Battery

02-0002

160 x 46.8 x 35mm

751

$48.07

$51.92

$51.92

8

4

Readytosky 1045 Propellers

04-0002

10 in x 4.5 deg

170

$16.89

$18.24

$18.24

9

1

HolyBro M9N GPS

02-0003

25 x 25 x 4mm

36.8

$76.64

$82.77

$88.77

10

1

FS-i6 Transmitter & FS-iA6B Receiver

02-0004

47 x 26.2 x 15mm

10

$46.00

$49.68

$59.53

11

1

Obstacle Avoidance Sensor for RG101 Pro Drone*

02-0006

~

~

$29.00

~

~

12

1

TELEMETRY RADIO DRONE 433MHZ

02-0005

~10 x 10 x 1.4mm

42

$43.56

$47.04

$54.04

13

1

Payload

03-0003

4.5” x 4.5” x 4”

453.59

~$10 (3D)

$10.80

$10.80

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CAD

Justin 20

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VIEWS

Justin 21

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Timeline

Alex 22

11/04/2025

PDR Review

11/12/2025

Final BOM - Place Part Orders

Winter Quarter

Test, Update, Validate POC

TBD Winter Quarter

Showcase

11/08/2025

CAD Model Completed

December

Proof of Concept Due

Winter Recess

(Concept Fabrication)

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Fabrication Plans

Alex 23

1. Frame Procurement

  • Purchase pre-built frame for strength and time efficiency
  • Verify motor mount spacing, payload clearance, and total mass

2. Component Selection

  • Motors, ESCs, and propellers sized for target thrust-to-weight ratio
  • Power system and communication hardware selected for compatibility

3. Flight Controller Integration

  • Mount existing Pixhawk/SpeedyBee on vibration isolation plate
  • Wire ESCs, GPS, telemetry, and radio link
  • Configure firmware (Mission Planner / QGroundControl) for autonomous modes

4. Payload Mechanism Fabrication

  • Design servo-actuated release using CAD
  • Manufacture via 3D printing
  • Mount with lightweight mounts and secure wiring�

5. Assembly & Wiring

  • Install propulsion, controller, and payload mechanism
  • Route power and signal lines neatly; verify electrical safety�

6. Testing & Validation

  • Test actuation and sensor calibration
  • Conduct hover test, waypoint mission, and payload drop trials

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Technical Concerns

Alex 24

Structural & Mechanical

  • Weight balance and CG shift during payload release
  • Frame vibration affecting sensors
  • Fastener loosening or fatigue over time�

Propulsion & Power

  • Motor/ESC sizing and overheating under load
  • Limited flight endurance due to battery sizing�

Avionics & Control

  • GPS or compass interference from wiring/payload

Payload Mechanism

  • Servo failure or unintended release
  • Power draw spikes from actuation
  • Drop stability and release timing�

Environmental & Safety

  • Overheating in sunlight or heavy load
  • Dust, rain
  • Flight safety, failsafes, and regulatory limits

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Thank You!

Justin 25

Quadcopter Payload Delivery - PDR