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Development of the Flight Guidance, Navigation, & Control System requires an understanding of the mission objectives and of how the FGN&C system must be designed to achieve these objectives-- for both hardware & software. The FCS requirements will be established from the mission objectives and from other applicable regulating sources (MIL Specs, FAA, JAA, ...). Trade studies will be performed to evaluate cost and technical feasibility-- from this, options will be selected and architectures will be formulated. Models will then be developed. Analysis and Simulation techniques will then be used to design the FCS control algorithms and develop the 6-DOF simulation. Once the control algorithms have been design and validated with the 6-DOF, hardware-in-the-loop (HITL) test & evaluation can begin-- near term this entails evaluating how the 6-DOF simulation flys the FCS hardware-- long term this entails migrating the FCS software from the 6-DOF into the appropriate FCS hardware units. Testing for requirements compliance is performed throughout the entire process. As each FCS hardware unit has been successfully completed the HITL test & eval phase, development of the configured equipment is finalized. At this point, the configured equipment can be installed into the aircraft and tested. Functional, Ground, and Flight testing is used to V&V the FCS on the aircraft. Qualification/ Certification testing is used to validate that the aircraft with the installed FCS meets the necessary requirements.

Seem complicated? It can be. But to minimize the cost and development of the FCS, it is essentially what must be done. This process, however, can be streamlined in many different ways-- maintaining those things that must be done, while cutting out chunks of costs and time.

Are you currently involved in an FCS development program? Have you got everything under control? Would you like to reduce costs and cut some time out of your program? We may be able to help.

A diagram of a typical Flight GN&C Analysis/Simulation/HITL Process is summarized below. Enjoy.

Note: To provide the necessary detail & maintain the flow, scrolling may be required. Sorry for any inconveniences.


Flight Control Analysis, Sim, & HITL Process Schematic (<6 sec download)


For more information on how ASTECH Engineering may be able to help you, please contact
Jeff Wilson at astech@cox.net or call 316-304-6157.

© Copyright 1996 ASTECH Engineering. All rights reserved. No part of this document may be
reproduced in any form without the expressed written consent of the author.

Keywords: Concept Research Development Integration Integrated Aviation Avionics Aircraft Flight Controls
Autopilots Navigation Guidance Analysis Simulation Software Algorithms Hardware Interfaces
Requirements Engineers HITL FCS GPS FMS UAV Systems