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K.D. Mease

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Web last revised:
August 3, 2007

 


University of California, Irvine

Current Research Projects

 

X-37

CEV Entry Guidance

We are developing entry guidance for Crew Exploration Vehicles (CEVs) and other future space vehicles that must be accurately and safely guided through the atmosphere. We have extended the Shuttle entry guidance concept to allow for crossrange as well as downrange trajectory planning. Prototype trajectory planning and trajectory tracking algorithms have been developed. Our Evolved Acceleration Guidance Logic for Entry (EAGLE) algorithm was independently tested in the Advanced Guidance and Control Study led by Marshall Space Flight Center and performed extremely well over a broad range of entry and abort scenarios for an X-33 type vehicle*.

Mars Landing

Future missions to Mars will require precise landing capability. We are working in collaboration with engineers at the Jet Propulsion Laboratory to develop guidance, navigation and control technology to enable precision landing.

Mars landing


Nonlinear Time Scales

The project objective is to develop a methodology for the analysis and design of nonlinear dynamical systems that have an underlying multiple time-scale structure. The presence of two or more widely separated time-scales offers the opportunity for reduced-order analysis and design, yet at the present time there is no general methodology for uncovering and exploiting time-scale separation in nonlinear systems.

(*) Picture obtained from www1.msfc.nasa.gov

 

 

The Henry Samueli School of Engineering

UCI

Dept. of Mechanical & Aerospace Engineering