Project

# Title Team Members TA Documents Sponsor
12 Anti-freeze water pipe system
Qinru Li
Rui Lan
Zichen Liang
Eric Clark design_document0.pdf
final_paper0.pdf
presentation0.pptx
proposal0.pdf
Introduction:
We noticed that in the winter when the temperature is below 0 degrees, the water pipe will become frozen. This will be a huge trouble if there are no people at home to deal with this trouble immediately. We are thinking to design a system which can monitor the temperature around the pipe. When the temperature is below the threshold, a heating system will start heating the system above a certain temperature to prevent the pipe from freezing. Meanwhile, the system will use a wifi module to inform the user about this issue.
This system is designed to operate outside the water pipe, so no penetration or any modification needed for the existing water pipe. The target of the water pipe is universal.

Components:
Sensor
We are going to use the temperature sensors for this system. We noticed that the temperature sensor today is accurate enough to detect changes in tenths unit. The temperature sensor will be installed on the outside of the water pipe because of the high thermal conductivity of most of the materials of water pipe (mostly steel, copper). The sensor should be insulated from our heating system by for example, take distance or insulating material between the two types of equipment.
Nevertheless, we are open-minded to an alternative sensor system which can improve our sensing accuracy. For example, the acoustic sensor may be considered to detect the state of water in the pipe because the speed of sound varies in the different density of matters.

Heating system
We plan to build the heater using thermal resistor rather than buying a product from the market. The heater uses DC voltage as the power supply. To do so, we are going to design an AC-DC conversion circuit using AC power straight from the building. The heating system also consists of a 12V battery such that when blackout exists, the AC voltage breaks down and the battery starts to work as an alternative.

Wifi module
When the temperature is below a certain level, we will send an alarm signal through a wifi module to an online server so that user can be immediately aware of the dangerous situation of the pipe.

Controller
The main functions of the controller are:
1) Decide when to turn on and off the heating system. In this part, we will apply a feedback control for safety reasons. When the water is overheated, the controller will shut up the heating and waiting for the temperature coming down again.
2) Send the alarm to the wifi module. We understand keeping heating up the water pipe is not feasible for a long time. Thus, we believe the system should warn the house owner once the temperature is below than the threshold.
3) Decide whether AC or battery power supply should be used. Note that besides the power base supply, the system also has a backup battery in the case of emergency.

Power System
We need AC-DC transformer to convert high-voltage AC power into DC power that the system components can use. We also need to design a voltage regulator such that we can convert the DC power to different scales for the requirements of different components in our circuit. Besides, a MUX is required to select the power from power panel (AC) and battery. The select signal will be sent by the controller


Web Board:
https://courses.engr.illinois.edu/ece445/pace/view-topic.asp?id=14561
https://courses.engr.illinois.edu/ece445/pace/view-topic.asp?id=14777

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.