Project

# Title Team Members TA Documents Sponsor
60 FadeX: Automated Nicotine Tapering Device
Ian Zentner
Justin Leith
Malik Kelly
Jiaming Xu design_document1.pdf
design_document2.pdf
proposal1.pdf
FadeX
**Team Members:**

* Malik Kelly (mkelly61)
* Justin Leith (jleit3)
* Ian Zentner (iwz2)

**Problem:**
Electronic cigarettes were originally marketed as cessation tools, yet they have become a primary source of addiction. Current cessation methods like gum or patches fail to address the "oral fixation" habit, leading to high relapse rates. Alternatively, "manual tapering" (buying bottles with progressively lower nicotine) is logistically difficult and prone to user error; users often relapse when they cannot find the specific lower concentration they need or struggle with the "cold turkey" steps between available concentrations (e.g., jumping from 5% down to 3%). There is currently no device that automates the tapering process while maintaining the user's behavioral routine.

**Solution:**
FadeX is a Bluetooth-enabled vaporization device that automates nicotine reduction. Unlike standard devices, FadeX utilizes a dual-reservoir system: one pod containing high-concentration nicotine and another containing zero-nicotine dilutant.
The device features an active mixing system using micro-peristaltic pumps driven by an ESP32 microcontroller. Based on a schedule set in the companion mobile app, the device calculates and delivers a specific ratio of liquids to the heating element in real-time. This allows for a continuous reduction in nicotine that is harder for the user to perceive (e.g., 5.0% to 4.9% to 4.8%) rather than distinct steps. The system includes pod authentication to ensure safe liquid usage and strict software fail-safes to limit dosage per hour. It would also implement safety protocols in regards to temperature, and have a charge-capability similar to that of current e-cigarettes.

**Solution Components:**

**Subsystem 1: Power & Energy Management**

* **Goal:** Get power in safely, regulate it, and budget it.
* **Power Source:** Samsung SDI INR18650-20S (1-cell Li-ion).
* **Charging:** TP5100 charging module. Premade circuit that powers Microcontroller.
* **User Wake/Enable:** Button to toggle vape back on after idle using watchdog timer.
* **Status/Low-Power Feedback:** RGB LEDs (Battery Low, Puffs Remaining, Error).

**Subsystem 2: Fluid, Mixture, and Sensing (The “Process Plant”)**

* **Goal:** Move liquid, know what’s happening, and control the blend.
* **Liquid Transport:** The Bartels Pump | BP7 × 2. Used to extract liquid from capsules and move into the central chamber to be atomized; isolates the liquid from mechanical parts.
* **Inhalation Detection:** BMP280 barometric pressure sensor or differential pressure sensor for airflow/puff detection.
* **Pump Drive / Ratio Control:** Dual H-Bridge driver (L9110S) used with PWM control to set relative pump rate.

**Subsystem 3: Thermal & Aerosol Generation**

* **Goal:** Turn the commanded dose into vapor consistently and safely.
* **Atomizer:** Standard resistance coil (Kanthal A1, ~1.0 Ω) wrapped in organic cotton.
* **Coil Switching/Drive:** N-channel MOSFET (IRLB3034) to fire the coil.
* **Overheat Protection:** NTC thermistor near coil/atomizer to monitor temperature and prevent overheating.

**Subsystem 4: Tapering Control, Display, and Connectivity Unit**

* **Central Control & Safety Logic:** Handles system state, permissions, and interlocks.
* **Microcontroller:** ESP32 (Wi-Fi/BLE for app connectivity).
* **Waveshare 2inch LCD Display Module:** To display analytics and options to user
* **Buttons:** user control of display and microcontroller logic

**Criterion For Success:**

* **Mixing Accuracy:** The device must produce a target nicotine concentration with a margin of error less than ±20%. 
* **Autonomous Tapering:** The system must successfully alter the concentration of nicotine over a specified amount of time, and use smaller or larger increments of stepping down based on the user’s settings (starting concentration value, time period of cessation) over a simulated timeframe without user intervention.
* **Safety & Limits:** The firmware must enforce a "lockout" if the user exceeds a set nicotine limit (e.g., >2mg in 1 hour) or if the coil temperature exceeds safe limits (>250°C).
* **Pod Security:** The device must refuse to fire if the pods are swapped (e.g., Nicotine pod inserted into the Dilutant slot) or if an unauthorized pod is detected.
* **Power conservation:** despite using power in more ways than the usual e-cigarette, the device should last for around 100 puffs, aiming for close to a full day on one charge.

ATTITUDE DETERMINATION AND CONTROL MODULE FOR UIUC NANOSATELLITES

Shamith Achanta, Rick Eason, Srikar Nalamalapu

Featured Project

Team Members:

- Rick Eason (reason2)

- Srikar Nalamalapu (svn3)

- Shamith Achanta (shamith2)

# Problem

The Aerospace Engineering department's Laboratory for Advanced Space Systems at Illinois (LASSI) develops nanosatellites for the University of Illinois. Their next-generation satellite architecture is currently in development, however the core bus does not contain an Attitude Determination and Control (ADCS) system.

In order for an ADCS system to be useful to LASSI, the system must be compliant with their modular spacecraft bus architecture.

# Solution

Design, build, and test an IlliniSat-0 spec compliant ADCS module. This requires being able to:

- Sense and process the Earth's weak magnetic field as it passes through the module.

- Sense and process the spacecraft body's <30 dps rotation rate.

- Execute control algorithms to command magnetorquer coil current drivers.

- Drive current through magnetorquer coils.

As well as being compliant to LASSI specification for:

- Mechanical design.

- Electrical power interfaces.

- Serial data interfaces.

- Material properties.

- Serial communications protocol.

# Solution Components

## Sensing

Using the Rohm BM1422AGMV 3-axis magnetometer we can accurately sense 0.042 microTesla per LSB, which gives very good overhead for sensing Earth's field. Furthermore, this sensor is designed for use in wearable electronics as a compass, so it also contains programable low-pass filters. This will reduce MCU processing load.

Using the Bosch BMI270 3-axis gyroscope we can accurately sense rotation rate at between ~16 and ~260 LSB per dps, which gives very good overhead to sense low-rate rotation of the spacecraft body. This sensor also contains a programable low-pass filter, which will help reduce MCU processing load.

Both sensors will communicate over I2C to the MCU.

## Serial Communications

The LASSI spec for this module requires the inclusion of the following serial communications processes:

- CAN-FD

- RS422

- Differential I2C

The CAN-FD interface is provided from the STM-32 MCU through a SN65HVD234-Q1 transceiver. It supports all CAN speeds and is used on all other devices on the CAN bus, providing increased reliability.

The RS422 interface is provided through GPIO from the STM-32 MCU and uses the TI THVD1451 transceiver. RS422 is a twisted-pair differential serial interface that provides high noise rejection and high data rates.

The Differential I2C is provided by a specialized transceiver from NXP, which allows I2C to be used reliably in high-noise and board-to-board situations. The device is the PCA9615.

I2C between the sensors and the MCU is provided by the GPIO on the MCU and does not require a transceiver.

## MCU

The MCU will be an STM32L552, exact variant and package is TBD due to parts availability. This MCU provides significant processing power, good GPIO, and excellent build and development tools. Firmware will be written in either C or Rust, depending on some initial testing.

We have access to debugging and flashing tools that are compatible with this MCU.

## Magnetics Coils and Constant Current Drivers

We are going to wind our own copper wire around coil mandrels to produce magnetorquers that are useful geometries for the device. A 3d printed mandrel will be designed and produced for each of the three coils. We do not believe this to be a significant risk of project failure because the geometries involved are extremely simple and the coil does not need to be extremely precise. Mounting of the coils to the board will be handled by 3d printed clips that we will design. The coils will be soldered into the board through plated through-holes.

Driving the inductors will be the MAX8560 500mA buck converter. This converter allows the MCU to toggle the activity of the individual coils separately through GPIO pins, as well as good soft-start characteristics for the large current draw of the coils.

## Board Design

This project requires significant work in the board layout phase. A 4-layer PCB is anticipated and due to LASSI compliance requirements the board outline, mounting hole placement, part keep-out zones, and a large stack-through connector (Samtec ERM/F-8) are already defined.

Unless constrained by part availability or required for other reasons, all parts will be SMD and will be selected for minimum footprint area.

# Criterion For Success

Success for our project will be broken into several parts:

- Electronics

- Firmware

- Compatibility

Compatibility success is the easiest to test. The device must be compatible with LASSI specifications for IlliniSat-0 modules. This is verifiable through mechanical measurement, board design review, and integration with other test articles.

Firmware success will be determined by meeting the following criteria:

- The capability to initialize, configure, and read accurate data from the IMU sensors. This is a test of I2C interfacing and will be tested using external test equipment in the LASSI lab. (We have approval to use and access to this equipment)

- The capability to control the output states of the magnetorquer coils. This is a test of GPIO interfacing in firmware.

- The capability to move through different control modes, including: IDLE, FAULT, DETUMBLE, SLEW, and TEST. This will be validated through debugger interfacing, as there is no visual indication system on this device to reduce power waste.

- The capability to self-test and to identify faults. This will be validated through debugger interfacing, as there is no visual indication system on this device to reduce power waste.

- The capability to communicate to other modules on the bus over CAN or RS422 using LASSI-compatible serial protocols. This will be validated through the use of external test equipment designed for IlliniSat-0 module testing.

**Note:** the development of the actual detumble and pointing algorithms that will be used in orbital flight fall outside the reasonable scope of electrical engineering as a field. We are explicitly designing this system such that an aerospace engineering team can develop control algorithms and drop them into our firmware stack for use.

Electronics success will be determined through the successful operation of the other criteria, if the board layout is faulty or a part was poorly selected, the system will not work as intended and will fail other tests. Electronics success will also be validated by measuring the current consumption of the device when operating. The device is required not to exceed 2 amps of total current draw from its dedicated power rail at 3.3 volts. This can be verified by observing the benchtop power supply used to run the device in the lab.