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2009-2011
Guidance, navigation and control system
Low-cost guidance systems for high-dynamic aircraft. Design, HW & SW development and implementation of an electro-optical terminal guidance system based on the recognition of a laser designator that pinpoints the target from the ground.
Real-time simulation of a flight system model, from laser signal attenuation to missile canard guidance and control, and real-world testing of laser-guided rockets at military facilities.
As part of the study, definition and design of the systems, AERTEC worked on terminal guidance.
We were also involved in the development and integration of the demonstrator (preparation of demonstrator tests; development of a technology demonstrator; functional tests on the demonstrator).
Innovation Director
