Carrier Recovery Enhancement for Maximum-Likelihood Doppler Shift Estimation in Mars Exploration Missions

被引:5
作者
Cattivelli, Federico S. [1 ]
Estabrook, Polly [2 ]
Satorius, Edgar H. [2 ]
Sayed, Ali H. [1 ]
机构
[1] Univ Calif Los Angeles, Dept Elect Engn, Los Angeles, CA 90095 USA
[2] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
基金
美国国家科学基金会;
关键词
Doppler effect; frequency estimation; maximum-likelihood estimation; space vehicle communication;
D O I
10.1109/JSTSP.2008.2005289
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
One of the most crucial stages of the Mars Exploration Missions is the Entry, Descent, and Landing (EDL) phase. During EDL, maintaining reliable communication from the spacecraft to Earth is extremely important for the success of future missions, especially in case of mission failure. EDL is characterized by very deep accelerations, caused by friction, parachute deployment and rocket firing among others. These dynamics cause a severe Doppler shift on the carrier communications link to Earth. Methods have been proposed to estimate the Doppler shift based on Maximum Likelihood. So far these methods have proved successful, but it is expected that the next Mars mission, known as the Mars Science Laboratory, will suffer from higher dynamics and lower SNR. Thus, improving the existing estimation methods becomes a necessity. We propose a Maximum Likelihood approach that takes into account the power in the data tones to enhance carrier recovery, and improve the estimation performance by up to 3 dB. Simulations are performed using real data obtained during the EDL stage of the Mars Exploration Rover B (MERB) mission.
引用
收藏
页码:658 / 669
页数:12
相关论文
共 21 条
[11]   Adaptive carrier tracking for direct-to-Earth Mars communications [J].
Lopes, C. G. ;
Satorius, E. ;
Sayed, A. H. .
2006 FORTIETH ASILOMAR CONFERENCE ON SIGNALS, SYSTEMS AND COMPUTERS, VOLS 1-5, 2006, :1042-+
[12]  
MITCHELTREE R, 2006, P IEEE AER C BIG SKY, P1
[13]   Communications blackout predictions for atmospheric entry of Mars Science Laboratory [J].
Morabito, David D. ;
Edquist, Karl T. .
2005 IEEE Aerospace Conference, Vols 1-4, 2005, :489-500
[14]  
PAPANDREOU A, 1994, 28 AS C SIGN SYST CO, V1, P50
[15]   SINGLE-TONE PARAMETER ESTIMATION FROM DISCRETE-TIME OBSERVATIONS [J].
RIFE, DC ;
BOORSTYN, RR .
IEEE TRANSACTIONS ON INFORMATION THEORY, 1974, 20 (05) :591-598
[16]  
SATORIUS E, 2003, 42153 JPL IPN
[17]  
SHAMSUNDER S, 1993, CONFERENCE RECORD OF THE TWENTY-SEVENTH ASILOMAR CONFERENCE ON SIGNALS, SYSTEMS & COMPUTERS, VOLS 1 AND 2, P1191, DOI 10.1109/ACSSC.1993.342383
[18]  
Udomkesmalee SG, 2005, AEROSP CONF PROC, P961
[19]   FREQUENCY ESTIMATION TECHNIQUES FOR HIGH DYNAMIC TRAJECTORIES [J].
VILNROTTER, VA ;
HINEDI, S ;
KUMAR, R .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1989, 25 (04) :559-578
[20]   Chirp parameter estimation from a sample covariance matrix [J].
Völcker, B ;
Ottersten, B .
IEEE TRANSACTIONS ON SIGNAL PROCESSING, 2001, 49 (03) :603-612