국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Simulation Framework for Rapid Entry, Descent, and Landing (EDL) Analysis : Volume 1
저자	Murri, Daniel G.
Keyword	ATMOSPHERIC ENTRY;; ATMOSPHERIC MODELS;; DESCENT;; MANNED MARS MISSIONS;; MONTE CARLO METHOD;; OPTIMIZATION;; SIMULATION;; SPACECRAFT LANDING;; SYSTEMS ANALYSIS;; TIME DEPENDENCE
URL	http://hdl.handle.net/2060/20100039818
보고서번호	NASA/TM-2010-216867/VOL1
발행년도	2010
출처	NTRS (NASA Technical Report Server)
ABSTRACT	The NASA Engineering and Safety Center (NESC) was requested to establish the Simulation Framework for Rapid Entry, Descent, and Landing (EDL) Analysis assessment, which involved development of an enhanced simulation architecture using the Program to Optimize Simulated Trajectories II (POST2) simulation tool. The assessment was requested to enhance the capability of the Agency to provide rapid evaluation of EDL characteristics in systems analysis studies, preliminary design, mission development and *****ution, and time-critical assessments. Many of the new simulation framework capabilities were developed to support the Agency EDL Systems Analysis (EDL-SA) team, that is conducting studies of the technologies and architectures that are required to enable higher mass robotic and human mission to Mars. The findings of the assessment are contained in this report.