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  <title><![CDATA[MS Proposal by Abinay J. Brown]]></title>
  <body><![CDATA[<p>Abinay J. Brown<br>(Advisor: Prof. Kyriakos Vamvoudakis)<br>will propose a master’s thesis entitled,<br>Real-Time Vision-Based Hazard Detection with Safe<br>Trajectory Optimization via Successive Convexification<br>for Lunar Landing<br>On<br>Wednesday, December 3rd at 2:00 p.m.<br>Montgomery Knight Building 317<br>Abstract<br>With the renewed interest in returning to the Moon, achieving autonomous and safe lunar descent and<br>landing is paramount for the success of future missions. Safe and autonomous descent also reduces the<br>overhead logistics of pre-planning, surveying, and mapping lunar landing sites. During the descent phase<br>of a lunar mission, the lander must steer away from rough terrain hazards and descend safely to the<br>surface while constrained by fuel, maneuverability, and localization uncertainty. This thesis presents a<br>framework for real-time state estimation, hazard detection from descent imagery, and safetyconstrained<br>trajectory optimization. The proposed framework navigates using dead reckoning and<br>Kalman filter-based sensor fusion to track the descent path using accelerometer and altimetry data<br>while leveraging image segmentation computer vision models to identify lunar hazards such as craters<br>and hills. Finally, a full-horizon minimum-time trajectory optimization problem with control and terminal<br>state constraints is approached using successive convexification (SCvx) optimization scheme. Hazardous<br>regions identified from descent imagery are represented as ellipse-based chance constraints enforced at<br>the terminal state, ensuring the lander avoids hazards with high confidence despite positional<br>uncertainty. The use of SCvx enables the decomposition of the nonlinear thrust vectoring dynamics and<br>constraints into a series of convex subproblems, significantly enhancing computational efficiency and<br>achieving real-time feasibility. This optimization is performed in a receding-horizon control loop,<br>allowing the lander to continuously reoptimize and adapt its descent trajectory in response to updated<br>hazard maps generated from real-time imagery. Simulations of the proposed framework are<br>implemented in a computer-generated 3D lunar environment to validate the approach.<br>Committee<br> Prof. Kyriakos Vamvoudakis – School of Aerospace Engineering (advisor)<br> Prof. Lu Gan– School of Aerospace Engineering<br> Prof. Glen Chou– School of Aerospace Engineering</p>]]></body>
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      <value><![CDATA[2024-12-03T14:00:00-05:00]]></value>
      <value2><![CDATA[2024-12-03T16:00:00-05:00]]></value2>
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      <value><![CDATA[Montgomery Knight Building 317]]></value>
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