RFI-5G Payload design

IGARSS_2023_Kband_RFI_Paper.pdf

Payload Structure

The payload is structured as a vertical stack of PCBs, like the rest of the satellite. This is done in order to be self-contained and to comply with the IEEE Open PocketQube Kit standard. 

This stack is designed so that the interferences from upper layers cannot penetrate down to the lower side and so the rest of the PocketQube. This isolation is mainly achieved thanks to the Structural piece, the aluminum shield, which connects the grounding from the PCBs in contact with it on both sides, so that it creates a grounded case, creating a Faraday Cage that is able to enclose the interferences radiated from within while also isolating those from the radiation coming from the exterior.

Another relevant structural component is the FR-4 Structural PCB. The only purpose of this PCB is to support the K-Band Antenna, which is very delicate and thin.

In both cases the Antenna and Top PCB with the FR-4 Structural and the Bottom PCB with the Interface they are attached with epoxy glue and soldered pins when possible. This ensures a good rigidity and a proper performance when faced the important vibrations produced during launch.

Payload Pinout

Schematics

Interface PCB

The Interface PCB is in charge of doing 3 main things:

This is why the interface schematic if divided into three parts.

low_freq_board.png

LDOs

This stage is in charge of regulating the 3.3V voltage line from the PQ to the various required voltage needed in the payload.

Voltage
Target component
2.5V
IF1Amp
2.7V
LNA2
2.75V

3V
 

To be finished

The schematic below shows the design of the voltage regulation circuit for the payload. The purpose of this circuit is to provide stable, regulated power at various voltage levels required by different components within the payload, which is essential for reliable and accurate signal processing and data collection.

Now an in-depth look at the decisions made in the design will be done:

1. Voltage Regulators (U4 and U5 - MIC2215 Series)
2. Decoupling Capacitors
3. Voltage Dividers and Feedback Networks
4. Separate Power Lines for Isolation

low_freq_board-LDOs.png

Voltage Boosters

This schematic provides a look at a voltage-boosting circuit. Here, three independent boost converter stages are built around the LT3048IDC-TRMPBF component (U1, U2, and U3). Each of these stages is responsible for generating a specific voltage required by various components in the payload, focusing on boosting an input voltage to a higher, stabilized output for sensitive RF systems.

Here is an expanded explanation of the design decisions and key aspects:

1. Boost Converter ICs (U1, U2, and U3 - LT3048IDC-TRMPBF)
2. Input Filtering Components (L1, L2, L3, C24, C25, C27)
3. Output Voltage Feedback and Resistor Networks
4. Output Decoupling and Stabilization (C3, C4, C7, C8, C11, C12)
5. Bypass Capacitors for Noise Reduction
6. Application-Specific Voltage Rails
7. Isolation Between Voltage Rails

low_freq_board-Boost1.png

Instrumentation Amplifier

This schematic shows an instrumentation amplifier stage used to process the voltage output from the RSSI (Received Signal Strength Indicator) block, which holds the scientific data from the payload. The amplifier conditions this signal so that it can be accurately digitized by the DAC input of the satellite's microcontroller.

Below is an expanded explanation of the main components and design choices within this stage:

1. Instrumentation Amplifier (U6 - AD8224ARZ-R7)
2. Gain Resistors (R15, R16, R17, and R18)
3. Input and Output Filtering (C21, C22, C26)
4. Voltage Divider for Signal Conditioning (R19, R20, R21, R22, R23)
5. RSSI Input and Output Connections

low_freq_board-Inst_amps.png

Bottom PCB

1. IF Input
2. First Amplification and Bandpass Filtering
3. Mixing

This is the most important part in the payload design

4. Second Amplification and Filtering
5. Additional Bandpass Filtering (SAW Filter)
6. RSSI Measurement

RFI-5G_RF_Bottom.png

Top PCB

RFI-5G_RF_Top.png

PCBs

This payload is structured in 4 main block as stated in the Payload block diagram page. We will start by explaining the Interface PCB.

Interface PCB

This board is charge of electrically connecting the payload to the rest of the satellite, redistributing the grounding and converting it to a Multiple Point Ground (MPG), more specifically into two points, a single pin on the bottom and a multiple consecutive pin array on the top. 

Bottom PCB

This board takes the IF signal from the Top PCB and downconverts it to be captured by the RSSI and output a voltage proportional to the signal power.

Top PCB

This board takes the signal from the antenna at the K Band and downconverts it to a Intermediate Frequency (IF).


Revision #3
Created 15 November 2024 18:47:49 by roger.almirall
Updated 15 November 2024 19:41:21 by roger.almirall