A Novel Loss Tolerant Data Transmission Schemes for Airborne Telemetry System of a Long Range Aerospace Vehicle

Received: 11 Feb 2022, Revised: 14 Feb 2022, Accepted: 05 May 2022, Available online: 26 May 2022, Version of Record: 26 May 2022

Karnati sudarsana Reddy; Lakshmi Boppanna; D. R. Jahagirdar

Abstract


The on-board telemetry system of an aerospace vehicle sends the vehicle performance parameters to the ground receiving station at all instances of its trajectory. During the course of its trajectory, the communication channel of a long range vehicle, experiences various phenomena such as plume attenuation, stage separation, manoeuvring of a vehicle and RF blackout, causing loss of valuable telemetry data. The loss of communication link is inevitable due to these harsh conditions even when using the space diversity of ground receiving systems. Conventional telemetry systems do not provide redundant data for long range aerospace vehicles. This research work proposes an innovative delay data transmission, frame switchover and multiple frames data transmission schemes to improve the availability of telemetry data at ground receiving stations. The proposed innovative schemes are modelled using VHDL and extensive simulations have been performed to validate the results. The functionally simulated net list has been synthesised with 130 nm ACTEL flash based FPGA and verified on telemetry hardware.
Operational scenario of a typical long range aerospace vehicle.

Operational scenario of a typical long range aerospace vehicle.
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Multiple frames data transmission.

Multiple frames data transmission.
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Architecture for redundant data transmission.

Architecture for redundant data transmission.
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FPGA Memory controller with external SDRAM memory.

FPGA Memory controller with external SDRAM memory.
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Test setup of Telemetry hardware with implemented schemes.

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Test setup of Telemetry



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https://www.researchgate.net/publication/357706762_A_Novel_Loss_Tolerant_Data_Transmission_Schemes_for_Airborne_Telemetry_System_of_a_Long_Range_Aerospace_Vehicle
      

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Conflict of interest


“Authors state no conflict of interest”


Funding Information


This research received no external funding or grants


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Peer review under responsibility of Defence Science Journal


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