Project

# Title Team Members TA Documents Sponsor
3 RFA: Smart Plant Pot
Gavin Tian
Morgan Sukalo
Trisha Murali
Surya Vasanth design_document1.pdf
other1.PDF
proposal1.pdf
proposal2.pdf
# **Smart** Plant Pot

**Team Members**
\- Morgan Sukalo (msukalo2)
\- Trisha Murali (tmurali2)
\- Gavin Tian (gtian3)

# **Problem**

Growing plants in any capacity is a maintenance intensive task and requires a lot of varying inputs and knowledge to accomplish successfully. Automating this process would be a step in automating agriculture in a controlled environment.

# **Solution**

Our solution is to build a hydroponic plant pot that can sustain and grow a plant from sprout or one that has been transplanted while automating all the processes associated with hydroponic plant care. It will have a variety of sensor and actuator based subsystems that perform action items related to hydroponic maintenance. We will then have a central control unit which will interpret all gathered data, and ensure an optimized growth environment. The user will be able monitor the current status of the plant and its environment via the UI subsystem. This system will display sensor data from every other subsystem, report issues requiring more intensive maintenance, and display existing conditions of the plant (example: humidity levels, water temperature, water levels), ultimately making hydroponic agriculture more user-friendly.

# **Solution** Components
*Diagram of System*
https://drive.google.com/file/d/1SQtptcK4uriIv2zN9ECVHA81-U5mPIS0/view

*Humidity Subsystem*
Most house plants need a humidity between 50-60% to protect against transpiration, and tropical plants require a higher humidity than this. The humidity subsystem will maintain a desired humidity level given the type of plant being grown and will consist of a variety of sensors/actuators to do so.

* We will have a humidity sensor (SHT35-DIS-F) which will constantly monitor the humidity within the Smart Pot. For the specified plant, this humidity will have to stay within a certain range, and the sensor will monitor this.
* On top of the clear lid for the pot, there will be an adjustable vent operated by a motor that will remain slightly open at all times to allow for air circulation, but if there is ever conditions that are not ideal to the plant (ex: humidity too high), the opening of the vent will adjust accordingly (ex: open up more to air out the plant if needed).
* All data will be sent to the central control unit. If the humidity is too low, a humidifier will be turned on until a desired humidity level is reached within the Smart Pot enclosure.
* If the humidity is too high, the vent at the top of the Smart Port enclosure will open wide, allowing for some of the gaseous water to escape (lowering humidity).

* SENSOR: humidity sensor for Smart Pot enclosure.
* ACTUATOR: humidifier, servo motor for vent @ top of enclosure
* CONTROL UNIT BEHAVIOR:

If the humidity is too high: open vent via servo motor

If humidity too low: turn on humidifier

*Oxygenation Subsystem*
For hydroponics, water needs to be oxygenated and agitated to facilitate plant growth and impede algae and bacteria.

* An air stone attached to a pump will be placed in the Smart Pot to continuously agitate the water.
* A small fan will be integrated into the side of the Smart Pot lid. This fan will push out the old air from inside of the enclosure.
* An air vent at the top of the Smart Pot enclosure will always be slightly open to allow fresh air into the enclosure. Closing/opening the air vent will be controlled by a servo motor. If the Smart Pot enclosure needs to be aired out, the vents can open wide.
* This system will be connected to the central control unit. The central control unit will allow the air stone to remain on all of the time. The fan will be turned on/off throughout the day as needed.

* SENSOR: n/a
* ACTUATOR: air stone, fan attached to wall of Smart Pot lid, servo motor for vent @ top of enclosure
* CONTROL UNIT BEHAVIOR:

The air stone will always be running.

The fan will only run during set intervals enforced by the control unit.

If airing-out of the Smart Pot is needed, the servo motor attached to the vents will be actuated to maximize Smart Pot air release.



*Grow Lights Subsystem*
As we know, plants require sunlight for growth. During winter, the amount of sunlight and other environmental factors a plant receives may not always be ideal. To offset this and provide for plant growth despite the season, we will be using grow lights.

* As part of this subsystem, we will also have light sensors to keep track of the amount of light the plant receives during a 24hr span. If this value ever becomes too high, the control unit will ensure that the LED growth light is off, and shades to shield the plant from light will be raised. If the control unit detects that the plant did not receive enough light, the LED growth light will be turned on for some amount of time until the light exposure requirement is fulfilled.

* SENSOR: light sensor for plant
* ACTUATOR: LED grow light (pre-made), shades with stepper motor
* CONTROL UNIT BEHAVIOR:

If the value tracked by light sensors become too high, grow light is turned off and shades move to cover the plant

If plant did not receive enough light, the LED grow light will be turned on and the shades will be moved out



*Water and Nutrient Subsystem*
Automated hydroponics requires a water and nutrient module to ensure water stability and sufficient nutrient levels. To deter algae and bacteria growth, water changes will need to be made every two weeks to ensure an optimized growth environment. This subsystem will monitor water level and water temperature.

* This is a gravity-based system and will include a water reservoir canister, a waste canister, and one nutrient canister.
* The water reservoir canister, nutrient canister and waste canister will be connected to the Smart Pot via 12V solenoid valves. Opening these valves will allow for the contents of one container to flow into the other.
* The water level of the Smart Pot will be monitored via a float switch (PLS-041A-3PAI), and a temperature sensor (DFR0198) will be used to observe the temperatures of the Smart Pot water and the water reservoir canister.
* If the water level falls below a specified threshold, the water reservoir temperature will be compared to the Smart Pot water temperature. If so, the valve connecting the water reservoir canister to the Smart Pot will be opened, and the Smart Pot will be filled to the desired level.
* Every two weeks, the water in the Smart Pot will be drained. Prior to draining, the temperature of the Smart Pot water and the water reservoir will be compared. If these values are similar, draining will commence.
* While the valve between the water reservoir and the Smart Pot remains closed, the valve between the Smart Pot and the waste canister will open when draining begins. All water from the Smart Pot will flow into the waste canister. This valve will then close, and the Smart Pot is refilled with freshwater from the water reservoir. Nutrients are then injected into the Smart Pot.

* SENSOR: temperature sensors, water level sensor (float sensor)
* ACTUATOR: Valves that are between all canisters and the Smart Pot
* CONTROL UNIT BEHAVIOR: will keep track of time passes since last water change, monitor water temperatures and water level. Will control when valves open/close.


*User Interface Subsystem*
The User Interface is a helpful feature for the users to track the environment of the plant.

* The user interface will allow the user to specify what plant type the user is currently trying to grow in the Smart Pot. These plant types will be displayed on a TFT LCD (DFR0664) and can be selected using a rotary encoder (PEC11R-4115F-S0018). Once selected, this information goes to the control unit, and all desired humidity levels, pH levels, light levels, etc. are set. The user interface will also display real time data coming from all of the sensors listed above. This gives the user information on the current status of their plant’s environment in the Smart Pot. In addition to this, any maintenance alerts will be displayed. This is where any alerts concerning manual overrides or human intervention will show. The overall idea here is that the rotary encoder will be used to browse through these different selections and the push button feature will be used to select an option.

* SENSOR: rotary encoder with push button feature
* ACTUATOR: TFT LCD screen to display real time temperature, humidity, etc. specs of Smart Pot
* CONTROL UNIT BEHAVIOR: display hydroponic plant types, plant status/stats, warning and alerts for the user



*Power Subsystem:*
The power subsystem aims to take wall power and convert it to voltages that are safe and usable for all sensors/actuators/devices that are needed to keep the Smart Pot up and running.

* The power system comprises a custom PCB with a step down IC, 12V DC wall adapter.
* The wall adapter is currently under contention as the amperage needs of the project need to be determined to pick the correct product.
* The PCB will route 12V and limit to the solenoids that control water flow as those require the highest voltage. It will also step down 12V to 3.3V DC for the microcontroller and sensors.

* SENSOR: n/a
* ACTUATOR: 12V, 3.3V, GND power rails
* CONTROL UNIT BEHAVIOR:

Step down voltages and supply power to all the subsystems

# **Criterion** For Success
The Smart Pot subsystems prove individual functionality as well as collaborative functionality. Ultimately, the Smart Pot will be able to sustain all subsystems and care for the plant for 4 weeks without human intervention.

To test, we want to check that all systems respond accurately and appropriately to their related sensor stimuli. The sensor readings themselves should match real life conditions in a reasonable manner and will be displayed on a UI for easy monitoring.

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.