Mission Performance Measures for Spacecraft Formation Flying

نویسندگان

  • Steven P. Hughes
  • Christopher D. Hall
چکیده

Clusters of low-performance spacecraft flying in formation may provide enhanced performance over single high-performance spacecraft. This is especially true for remote sensing missions where interferometry or stereographic imaging may provide higher resolution data. The configuration of such formations vary during an orbit due to orbital dynamics, and over larger time scales due to perturbations. Selection of a configuration should be based on overall performance of the formation. In this paper, performance measures are developed and evaluated based on integration over one orbit. The measures involve angular separation of spacecraft, instantaneous overlap access area, and an area-based measure of the separation of the spacecraft. An optimization scheme is used to determine the best configuration for a four-spacecraft formation.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits

The problem of relative motion control for spacecraft formation flying in eccentric orbits is considered in this paper. Due to the presence of nonlinear dynamics and external disturbances, a robust fuzzy sliding mode controller is developed. The slopes of sliding surfaces of the conventional sliding mode controller are tuned according to error states using a fuzzy logic and reach the pre-define...

متن کامل

Navigation Performance Predictions for the Orion Formation Flying Mission

This paper presents hardware-in-the-loop results that experimentally demonstrate precise relative navigation for true formation flying spacecraft applications. The approach is based on carrier-phase differential GPS, which is an ideal navigation sensor for these missions because it provides a direct measure of the relative positions and velocities of the vehicles in the fleet. In preparation fo...

متن کامل

Formal Specification and Design of Fault-Tolerant Satellite Formation Flying System

The satellite formation flying system is a collaborative system where multiple satellites cooperate in a formation to perform consensus mission in space LEO (Low-Earth-Orbit) through librations points. In recent years, this kind of formation flying systems are getting attention because of reduced cost of mission, failures and recovery and flexibility. If one big spacecraft is at a mission and i...

متن کامل

Annual AIAA/USU Conference on Small Satellites Drift Recovery and Station Keeping Results for the Historic CanX-4/CanX-5 Formation Flying Mission

Specialized drift recovery and station keeping algorithms were developed for the Canadian Advanced Nanospace eXperiments 4 and 5 (CanX-4 & CanX-5) formation flying mission (launched 30 June 2014), and successfully verified on orbit. These algorithms performed almost exactly according to predictions. The highly successful CanX4 and CanX-5 formation flying demonstration mission was completed in N...

متن کامل

Emerald: A Low-Cost Spacecraft Mission for Validating Formation Flying Technologies

Spacecraft formation flying is a proposed technology with vast performance implications ranging from enhanced mission capabilities to radical reductions in operations cost. To explore this concept and to enable its realization, Stanford University and Santa Clara University have initiated development of a simple, low cost, twosatellite mission known as Emerald. The Emerald mission has four prim...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 1999