Serial Implementations of Flight Termination Systems

April 26, 2018 | BY: Paul Cook

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Flight safety is taken seriously in every aerospace application with rigorous regulations and training mandated for operating aircraft. Safety is also critical for unmanned military systems, such as UAVs, missiles and targets. These are typically fitted with a flight termination system (FTS). The purpose of such a system is to allow an individual, such as a range safety officer, to terminate the flight of a vehicle if it presents a risk to people or property.

It's important that the FTS operates reliably – if there is any reasonable chance it may fail to operate then a flight should be aborted. One way to provide assurance that such systems are working correctly is to monitor all data from the FTS. In an ideal world, a range safety officer would have constant access to real-time built in test (BIT) information from each element of the FTS.

In reality, getting comprehensive data creates complications – especially for missiles as space and mass are critically short on supply. All this extra information must be packaged, encoded and sent to ground. In a traditional safety system this typically means extra wiring is required for each parameter. This wiring is heavy, costly and creates a system that is more difficult to install and maintain.

This is partly due to the fact that traditional FTS have parallel wiring strategies, thus one way to address the problem of extra wiring is to move from a parallel wiring system to a serial one. It is possible to implement this by using a multidrop bus i.e. a bus where all hardware is connected to a single electrical circuit.

A Multi-Drop Configuration uses far fewer wires to interconnect an FTS

Curtiss-Wright has approached the design of its FTS systems to facilitate the wants and needs of range safety officers, and indeed, telemetry engineers. To this end, all our RF products are DSP based designs that offer a microcontroller  interface for programming and configuration. They also provide status information such as tone, ARM, termination and SSTO status. You can learn more about this topic by reading the white paper “Non-Traditional Implementation of a Traditional Safety System”.

Author’s Biography

Paul Cook

Director of Missile Systems, Curtiss-Wright Defense Solutions

Paul Cook is the Director of Missile Systems at Curtiss-Wright Defense Solutions. He has 37 years of extensive design and product line experience in Telemetry Systems. He has held both engineering and management positions in Design & Development, Embedded Encryption, RF Subsystems and Data Links, Engineering & Business Management, and Program Management. He has 34 years of experience in the Telemetry industry and 3 years in Information Assurance Type I CCEP certifications. Paul joined Teletronics in 2007 and in addition, worked in the Telemetry Industry for General Dynamics Corporation, Aydin Corporation, and L-3 Communications Corporation. Paul obtained a BS degree from The College of New Jersey and has various postgraduate courses towards a MBA and Program Management Certifications.

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