@conference {35,
	title = {Low Cost Rapidly Reconfigurable UAV Autopilot for Research and Development of Guidance, Navigation and Control Algorithms},
	booktitle = {ASME/IEEE MESA09},
	year = {2009},
	month = {08/2009},
	publisher = {International Conference on Mechatronic and Embedded Systems and Applications},
	organization = {International Conference on Mechatronic and Embedded Systems and Applications},
	address = {San Diego, CA},
	author = {Mariano Lizarraga and Gabriel H Elkaim and Gregory Horn and Ren Curry and V Dobrokhodov and I Kaminer}
}
@conference {36,
	title = {Simulink Based Hardware-in-the-Loop Simulator for Rapid Prototyping of UAV Control Algorithms},
	booktitle = {AIAA Infotech Conference},
	year = {2009},
	month = {08/2009},
	address = {Seattle, WA},
	author = {Mariano Lizarraga and V Dobrokhodov and Gabriel H Elkaim and Ren Curry and I Kaminer}
}
@conference {37,
	title = {Aerial Photography using a Nokia N95},
	booktitle = {WCECS2008},
	year = {2008},
	note = {Certificate of Merit Award},
	month = {10/2008},
	publisher = {World Congress on Engineering and Computer Science},
	organization = {World Congress on Engineering and Computer Science},
	address = {San Francisco, CA},
	author = {David Ilstrup and Mariano Lizarraga and Gabriel H Elkaim and J Davis}
}
@proceedings {43,
	title = {Comparison of Low-Cost GPS/INS Sensors for Autonomous Vehicle Applications},
	year = {2008},
	pages = {285-293},
	address = {Monterey, CA},
	author = {Gabriel H Elkaim and Mariano Lizarraga and L Pedersen}
}
@conference {16,
	title = {MACH-1: Control System Modeling and Design for a Mars Flyer},
	booktitle = {AIAA GNC 2008},
	year = {2008},
	month = {08/2008},
	publisher = {AIAA},
	organization = {AIAA},
	address = {Honolulu, HI},
	abstract = {Mars science missions would benefit from the ability to acquire high resolution images of the Martian surface, as well as sensor coverage from other sensors. A robotic aircraft on Mars has been proposed to carry these instruments. The atmosphere and weak Martian gravity make the plane equivalent to a very high altitude aircraft on the Earth. The MACH-1 challenge is a design contest to model, simulate, and design the control system for this future Mars flyer. The design specifications are used to create a SIMULINK full six degree of freedom model, which is validated with open loop simulations. Trim conditions are used to generate perturbation models for control loop design, and output regulator linear quadratic regulator design is used to generate a gain matrix for straight and level flight. The generated model is unstable, and the control design developed cannot stabilize the non-linear model.},
	author = {Gabriel H Elkaim and J.-W. Choi and Daniel Garalde and Mariano Lizarraga}
}
@proceedings {42,
	title = {Spatially Deconflicted Path Generation for Multiple UAVs in a Bounded Airspace},
	year = {2008},
	pages = {633-640},
	address = {Monterey, CA},
	author = {Mariano Lizarraga and Gabriel H Elkaim}
}
