Project

# Title Team Members TA Documents Sponsor
65 Active Postural Correction Vest
 Aparna Srinivasan
Jordyn Andrews
Sophia Sulkar
 Frey Zhao proposal1.pdf
# Active Postural Correction Vest


**Team Members:**
- Aparna Srinivasan (aparnas3)
- Jordyn Andrews (jandr25)
- Sophia Sulkar (ssulkar2)


# Problem


Poor posture is an extremely common issue in modern society, especially in the workplace, where employees sit and slouch for hours on end. Long-term slouching can lead to musculoskeletal imbalances, chronic back pain, and reduced respiratory efficiency. Existing solutions are either braces (which do not require any muscular effort from the person) or simple notification (devices that buzz but do not actually enforce correction). There is a lack of active solutions that physically assist the user in regaining proper posture without requiring constant conscious effort, or just doing all the work for them with no effort at all.


# Solution


We propose an Active Postural Correction Vest. Unlike passive braces, this system uses an active electromechanical feedback loop to physically retrain the user’s posture, while also letting go so that good posture is maintained by the user, not just the device itself.


The device consists of a wearable vest equipped with stretch sensors which attach to elastics. These sensors continuously monitor how much the elastics are extended. When the system detects a "slouch" state (shown by the stretch sensor reading shifting away from the calibrated threshold), the central PCB triggers a high-torque servo motor mounted on the back plate. The servo reels in a cabling system made of elastic connected to the shoulder straps, physically pulling the user's shoulders back into a proper position. Once the sensors detect that the user has returned to the correct posture, the servo releases tension, allowing for natural movement and self-maintained posture until the next slouch event.


In terms of safety precautions, we plan to create an assistive device that does not use a lot of force, so it cannot cause any damage. We also are going to have an emergency stop button as well as an auto shut-off when the resistance level reaches a level that is too high. We also will filter out noise by adding a timer that only activates the motors if the person is sitting in a slouched position for a prolonged time.




# Solution Components


## Subsystem 1


**Sensing and Input**
This subsystem is responsible for detecting the user's postural state by measuring the tension and force exerted by the brace straps against the body.
- Primary Sensors (Stretch Subsystem): We will use stretch sensors placed between the shoulder strap and the user's clavicle. When the user is well-postured, the straps are taut (indicated by high Resistance/Voltage). When slouching, the straps loosen or shift (indicated by low Resistance/Voltage).
- Secondary Sensor (Pressure Subsystem): We will also use pressure sensors on the front of the vest to provide a safety check to make sure that the strap tension stays within a comfortable limit


## Subsystem 2
**Mechanical Correction**
This subsystem provides the physical force required to retract the shoulders.
- Actuator: We will use a Servo motor, which will be able to reel in the elastic band without being too powerful or dangerous.
- Mechanism: The servo will be mounted on a central back plate, which could be 3D printed, using a spool-and-cable mechanism to shorten the effective length of the shoulder straps.
## Subsystem 3
**Control & Power**
This subsystem processes sensor data and drives the motor.
- Microcontroller: possibly an ESP32 for wireless support
- Power Regulation: batteries, etc.
- Failsafe: Kill switch/button


## Subsystem 4
**Bluetooth App**
A Bluetooth-connected app will display posture behavior over time (how often and how long the user slouches). The app would also allow adjustment of sensitivity and comfort limits, and let the user switch between training and brace modes.

# Criterion For Success

- The system shall detect a slouched posture when the stretch sensor output drops below a calibrated upright threshold for >= 30 seconds.

- Normal movements such as walking, reaching, or twisting shall not trigger motor actuation during a 10-minute movement test.

- When a slouch is detected, the servo shall retract the shoulder straps by a fixed amount of mm within 10 -15 seconds, resulting in visible shoulder retraction.

- The servo shall fully release strap tension within 5 seconds after the stretch sensor returns above the upright threshold.

- Strap pressure shall remain below a predefined safe limit, and the system shall disable the motor immediately when the emergency stop button is pressed.

- The vest shall operate continuously for at least 4 hours on battery power while maintaining full sensing and actuation functionality.

Illini Voyager

Cameron Jones, Christopher Xu

Featured Project

# Illini Voyager

Team Members:

- Christopher Xu (cyx3)

- Cameron Jones (ccj4)

# Problem

Weather balloons are commonly used to collect meteorological data, such as temperature, pressure, humidity, and wind velocity at different layers of the atmosphere. These data are key components of today’s best predictive weather models, and we rely on the constant launch of radiosondes to meet this need. Most weather balloons cannot control their altitude and direction of travel, but if they could, we would be able to collect data from specific regions of the atmosphere, avoid commercial airspaces, increase range and duration of flights by optimizing position relative to weather forecasts, and avoid pollution from constant launches. A long endurance balloon platform also uniquely enables the performance of interesting payloads, such as the detection of high energy particles over the Antarctic, in situ measurements of high-altitude weather phenomena in remote locations, and radiation testing of electronic components. Since nearly all weather balloons flown today lack the control capability to make this possible, we are presented with an interesting engineering challenge with a significant payoff.

# Solution

We aim to solve this problem through the use of an automated venting and ballast system, which can modulate the balloon’s buoyancy to achieve a target altitude. Given accurate GPS positioning and modeling of the jetstream, we can fly at certain altitudes to navigate the winds of the upper atmosphere. The venting will be performed by an actuator fixed to the neck of the balloon, and the ballast drops will consist of small, biodegradable BBs, which pose no threat to anything below the balloon. Similar existing solutions, particularly the Stanford Valbal project, have had significant success with their long endurance launches. We are seeking to improve upon their endurance by increasing longevity from a power consumption and recharging standpoint, implementing a more capable altitude control algorithm which minimizes helium and ballast expenditures, and optimizing mechanisms to increase ballast capacity. With altitude control, the balloon has access to winds going in different directions at different layers in the atmosphere, making it possible to roughly adjust its horizontal trajectory and collect data from multiple regions in one flight.

# Solution Components

## Vent Valve and Cut-down (Mechanical)

A servo actuates a valve that allows helium to exit the balloon, decreasing the lift. The valve must allow enough flow when open to slow the initial ascent of the balloon at the cruising altitude, yet create a tight seal when closed. The same servo will also be able to detach or cut down the balloon in case we need to end the flight early. A parachute will deploy under free fall.

## Ballast Dropper (Mechanical)

A small DC motor spins a wheel to drop [biodegradable BBs](https://www.amazon.com/Force-Premium-Biodegradable-Airsoft-Ammo-20/dp/B08SHJ7LWC/). As the total weight of the system decreases, the balloon will gain altitude. This mechanism must drop BBs at a consistent weight and operate for long durations without jamming or have a method of detecting the jams and running an unjamming sequence.

## Power Subsystem (Electrical)

The entire system will be powered by a few lightweight rechargeable batteries (such as 18650). A battery protection system (such as BQ294x) will have an undervoltage and overvoltage cutoff to ensure safe voltages on the cells during charge and discharge.

## Control Subsystem (Electrical)

An STM32 microcontroller will serve as our flight computer and has the responsibility for commanding actuators, collecting data, and managing communications back to our ground console. We’ll likely use an internal watchdog timer to recover from system faults. On the same board, we’ll have GPS, pressure, temperature, and humidity sensors to determine how to actuate the vent valve or ballast.

## Communication Subsystem (Electrical)

The microcontroller will communicate via serial to the satellite modem (Iridium 9603N), sending small packets back to us on the ground with a minimum frequency of once per hour. There will also be a LED beacon visible up to 5 miles at night to meet regulations. We have read through the FAA part 101 regulations and believe our system meets all requirements to enable a safe, legal, and ethical balloon flight.

## Ground Subsystem (Software)

We will maintain a web server which will receive location reports and other data packets from our balloon while it is in flight. This piece of software will also allow us to schedule commands, respond to error conditions, and adjust the control algorithm while in flight.

# Criterion For Success

We aim to launch the balloon a week before the demo date. At the demo, we will present any data collected from the launch, as well as an identical version of the avionics board showing its functionality. A quantitative goal for the balloon is to survive 24 hours in the air, collect data for that whole period, and report it back via the satellite modem.

![Block diagram](https://i.imgur.com/0yazJTu.png)