국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Simulation of Attitude and Trajectory Dynamics and Control of Multiple Spacecraft
저자	Stoneking, Eric T.
Keyword	SIMULATION;; SPACECRAFT CONTROL;; SPACECRAFT MODELS;; SYSTEMS ENGINEERING;; SPACECRAFT TRAJECTORIES;; ATTITUDE CONTROL;; APPLICATIONS PROGRAMS (COMPUTERS); ORBIT PERTURBATION;; TORQUE;; FEASIBILITY;; CONTROL THEORY;; ATMOSPHERIC DENSITY;;
URL	http://hdl.handle.net/2060/20090032130
보고서번호	GSC-15737-1
발행년도	2009
출처	NTRS (NASA Technical Report Server)
ABSTRACT	Agora software is a simulation of spacecraft attitude and orbit dynamics. It supports spacecraft models composed of multiple rigid bodies or flexible structural models. Agora simulates multiple spacecraft simultaneously, supporting rendezvous, proximity operations, and precision formation flying studies. The Agora environment includes ephemerides for all planets and major moons in the solar system, supporting design studies for deep space as well as geocentric missions. The environment also contains standard models for gravity, atmospheric density, and magnetic fields. Disturbance force and torque models include aerodynamic, gravity-gradient, solar radiation pressure, and third-body gravitation. In addition to the dynamic and environmental models, Agora supports geometrical visualization through an OpenGL interface. Prototype models are provided for common sensors, actuators, and control laws. A clean interface accommodates linking in actual flight code in place of the prototype control laws. The same simulation may be used for rapid feasibility studies, and then used for flight software validation as the design matures. Agora is open-source and portable across computing platforms, making it customizable and extensible. It is written to support the entire GNC (guidance, navigation, and control) design cycle, from rapid prototyping and design analysis, to high-fidelity flight code verification. As a top-down design, Agora is intended to accommodate a large range of missions, anywhere in the solar system. Both two-body and three-body flight regimes are supported, as well as seamless transition between them. Multiple spacecraft may be simultaneously simulated, enabling simulation of rendezvous scenarios, as well as formation flying. Built-in reference frames and orbit perturbation dynamics provide accurate modeling of precision formation control.