Trajectory estimation for aircraft with incomplete measurements
CSTR:
Author:
Affiliation:

(The PLA Unit 91550, Dalian 116023, China)

Clc Number:

TP274

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    A new estimation method based on sparse optimization was proposed. This method alleviated the ill-posedness by decreasing the dimension of parameter space. The sparse representation of the trajectory was achieved by using the B-spline function. An optimization model for trajectory estimation was constructed according to the relationship between the measurement data and the trajectory, and was solved by using the Gauss-Newton method. In this model, the number of the parameters to be estimated was determined by the number of the spline knots. A sparse optimization model for optimal knot selection was established by using the discontinuity of high order derivative of spline at the knots. This model was solved by using a convex optimization approach, and the number of knots was minimized. Simulation results showed that the sparse optimization method can dramatically improve the estimation accuracy of trajectory during the incomplete measured interval.

    Reference
    Related
    Cited by
Get Citation

LI Dong, LIU Xue. Trajectory estimation for aircraft with incomplete measurements[J]. Journal of National University of Defense Technology,2020,42(1):117-124.

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:September 12,2018
  • Revised:
  • Adopted:
  • Online: January 19,2020
  • Published: February 28,2020
Article QR Code