Integrated Performance of an Autonomous Optical Navigation System for Space Exploration

Author(s):  
John Christian ◽  
E. Glenn Lightsey
2014 ◽  
Vol 629 ◽  
pp. 321-326
Author(s):  
Javaan Chahl ◽  
Aakash Dawadee

Navigation by means that are fully self contained, without the weight and cost of high performance inertial navigation units is highly desirable in many applications both military and civilian. In this paper we introduce a suite of sensors and behaviors that include: the means to reduce lateral drift due to wind using optical flow, detection of a constellation of landmarks using a machine vision system, and a polarization compass that is reliable at extreme latitudes based on polarization. In a series of flight trials and detailed simulations we have demonstrated that a combination of these functions achieves purely optical navigation with simplicity and robustness.


2017 ◽  
Vol 50 (1) ◽  
pp. 11658-11663
Author(s):  
Mikhail N. Matveev

2017 ◽  
Vol 10 (2) ◽  
pp. 147-156 ◽  
Author(s):  
T. Franz ◽  
D. Lüdtke ◽  
O. Maibaum ◽  
A. Gerndt

2013 ◽  
Vol 11 (6) ◽  
pp. 1196-1203 ◽  
Author(s):  
Dae Hee Won ◽  
Sebum Chun ◽  
Seung-Woo Lee ◽  
Sangkyung Sung ◽  
Jiyun Lee ◽  
...  

Sensors ◽  
2019 ◽  
Vol 19 (19) ◽  
pp. 4064 ◽  
Author(s):  
John Christian

Future space exploration missions require increased autonomy. This is especially true for navigation, where continued reliance on Earth-based resources is often a limiting factor in mission design and selection. In response to the need for autonomous navigation, this work introduces the StarNAV framework that may allow a spacecraft to autonomously navigate anywhere in the Solar System (or beyond) using only passive observations of naturally occurring starlight. Relativistic perturbations in the wavelength and direction of observed stars may be used to infer spacecraft velocity which, in turn, may be used for navigation. This work develops the mathematics governing such an approach and explores its efficacy for autonomous navigation. Measurement of stellar spectral shift due to the relativistic Doppler effect is found to be ineffective in practice. Instead, measurement of the change in inter-star angle due to stellar aberration appears to be the most promising technique for navigation by the relativistic perturbation of starlight.


2013 ◽  
Vol 36 (6) ◽  
pp. 1576-1595 ◽  
Author(s):  
S. D’Amico ◽  
J.-S. Ardaens ◽  
G. Gaias ◽  
H. Benninghoff ◽  
B. Schlepp ◽  
...  

Author(s):  
A. M. Kovalenko ◽  
A. A. Shejnikov

In article approaches to creation of the complex inertial and optical navigation system of the short-range tactical unmanned aerial vehicle are considered. Algorithms constant and periodic (in intermediate points of a route) are offered correction of the platformless onboard inertial navigation system. At integration of information on parameters of the movement of the unmanned aerial vehicle (received from the considered systems) the invariant loosely coupled scheme of data processing on the basis of the expanded filter of Kallman was used that allowed to lower significantly a systematic component of an error of the platformless inertial navigation system. Advantages of the complex inertial and optical navigation system when ensuring flight of the unmanned aerial vehicle in an area of coverage of means of radio-electronic fight of the opponent are shown. The results of modeling confirming a possibility of ensuring precision characteristics of the inertial and optical navigation system in the absence of signals of satellite radio navigational systems are presented.


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