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Autopilot Design Points of Discussion
Simulation regarding Autopilot modes. Results generated. 6 Degree of freedom model designed for nonlinear simulation. Conclusion and Plan of action. Shihan Tissera Preliminary Design Review 1st March 2012
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Combined Glideslope and Flare block diagram
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Combined result of Glideslope and Flare
Enlarged section Height(m) Combined result of Glideslope and Flare Time(s)
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Conclusion and Action Plan
The current simulation results show the controllers obtained, works well for the reduced order model in the case of landing and height acquire/hold modes. Further testing will be carried out by integrating the developed linear autopilot to the nonlinear 6DOF model. After the integration the PID controllers will be re-tuned for better results.
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