Pinaka Aerospace Solutions Private Limited Kalyan Nagar, Bangalore, Karnataka

The synchro card in ATE is capable of generating six outputs synchro signals and six reference channels (one used and five spare). The synchro output channels generated by ATE will be having a step size of at least 15°. All the synchro channels will be routed through ATE control panel. Also, these will be available at patch panel for monitoring using synchro display. The synchro card generates synchro output signals on receiving commands from FPGA based I/O card. The FPGA I/O card is used as interface between IPC and synchro output card. The synchro card is capable of generating 3 phase synchro channels and single phase synchro reference signals. The angle set at GUI will be read by host software and send to FPGA card as commands. FPGA card sets the data bits (I/O bits) for generation of synchro outputs by synchro card.

8548 based SBCs Single Board Computer(SBC) is a complete computer built on a single circuit board, with processor(s), memory, input/output (I/O) and other features like CPU – i74790S, 8GB DDR3 RAM @ 1333MHz, 500GB SATA HDD, Graphics Controller – Chipset Integrated Intel HD Graphics, Ethernet Interface – 10/100/1000 Mbps, SBC Form Factor: - Full Size, Slot CPU Card.

Pinaka has designed and developed a generic, CRI-certified microcontroller based "No Volts cum Pulse Tester" for fighter aircrafts that detects the presence of stray voltages. It also detects the correctness of amplitude and the duration of the firing pulses. The system is in operational use with ADA and HAL. This product of Pinaka demonstrate our ability to develop products in the realm of embedded hardware and software from design and development to testing and certification.

Specifications Records Impact Events: Max Peaks X, Y, and Z; Internal Temperature; Battery Level Built in temperature sensor Sensors record direction, amplitude Serial or USB data transfer options Self-contained unit design, free of cables and wires Up to 24 months of battery life LED operation, single tap and double tap status indicators Programmable display time on impact.

The DOUT card generates discrete output signals on receiving commands from FPGA based I/O card. The FPGA I/O card is used as interface between IPC and DOUT card. The logic levels set at GUI will be read by host software and send to FPGA card as commands. FPGA card will be setting the data bits (I/O bits) for generation of discrete outputs by DAC card.

The DIN card takes discrete input signals, converts into data bits (1 or 0 according to the input logic level) and transfers to FPGA based I/O card. The FPGA I/O card is used as interface between IPC and DIN card. The host software receives the binary data from FPGA card and displays on GUI.

The Digital TGT Control Amplifier is a digital fit, form and functional replacement for the original Analog TGT amplifier of the MK-804, MK811 and MK871 engines of the Jaguar and Hawk aircraft. The Digital TGT Amplifier is a mature and field proven system. The Speed and temperature(TGT) amplifier controls a solenoid valve in the fuel–flow system. For a given throttle setting, the fuel-flow is controlled depending on defined external pressure and temperature conditions. Features Compatible with Mk-804, Mk-811 and Mk-871 engines Full digital system Monitors engine parameters (RPM, TGT and TGT counter) Simple flight-line aircraft retrofit - No Aircraft modifications required Advanced self-BIT (Built-In-Test): Tests all DTGT functions, modules and engine sensors Optional monitoring capabilities of more engine parameters Flight-line re-programmable RS 485 Communication (Real time Monitoring) Open thermocouple detecting

Data Field Loader (DFL) Pinaka has designed and developed a Universal Data Field Loader for uploading and downloading Mission and Navigation data. It is also capable of providing the following functions for the Pilot/Maintenance Engineer and Mission Planner. Pilot / Maintenance Engineer: The Pilot/Maintenance Engineer can use DFL as briefing and de-briefing tool, prepare missions, analyse system performance, analyse techniques, replay missions, perform Built-in-Test, check serviceability of the entire system and LRU/SRU level checks of the system. Mission Planner: The mission planner can use DFL to perform automatic analysis of the downloaded data, programming of various techniques and use it as briefing and de-briefing tool for the pilots.

Pinaka has designed and developed the signal conditioning cards for testing of various IFCS vanes/sensors/probes of LCA such as AOA/AOSS, ASA, CSRP, DCSU, FCP, RSA, TAT for generation of required voltages/currents for excitation of UUT and measurement circuits for UUT response. Data acquisition is implemented for RVDT/LVDT Interfaces, Discrete Inputs and Analog Inputs. The signal conditioning boards also generate required drive signals (ON/OFF) for the GO/NO-GO lamps that indicate final clearance of the unit after comprehensive diagnostics and health checks.  

PA9636+ Controller Board The controller board is configured around Tiva™ TM4C123GH6PGE Microcontroller of Texas Instruments. The controller PCB consists of the microcontroller, two 16-bit ADCs, another microcontroller configured for implementing Ethernet MAC/PHY 10/100, Serial EEPROM and OLED Display. The controller board can be used as general purpose interface board for data acquisition using configurable interfaces such as Discrete I/Os, Analog Inputs, RS 232, RS 422/485, CAN, USB and Ethernet communication interfaces. Interface to SD card is also available for reading external data.

The DAC card generates analog output signals on receiving commands from FPGA based I/O card. The FPGA I/O card is used as interface between IPC and DAC card. The DAC card is capable of generating single ended voltages of both unipolar and bipolar types. The analog values will be set at GUI, which will be read by host software and will be sent to FPGA card as commands. FPGA card will be setting the data bits (I/O bits) for generation of analog outputs by DAC card.