Guidance and Navigation System Design for a Ship Self Defense Missile

Guidance and Navigation System Design for a Ship Self Defense Missile

Author(s):

E. Ohlmeyer ( Naval Surface Warfare Center , Dahlgren, VA )
J. Bibel
C. Phillips
S. Reiman

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Guidance Navigation and Control Conference

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-6702

Paper no.:

AIAA Paper 2006-6702

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200619 [CD-ROM 2006 Disc 19]

Type:

Technical Paper

Details

TDL ID:	ZA00047246
Series ID:	PA00000153
Conf. info. (Name):	AIAA Guidance, Navigation, and Control Conference and Exhibit
Conf. info. (Number):	2006
Conf. info. (Venue):	Keystone, Colorado
Conf. info. (Date):	2006.08.21-2006.08.24

Similar Items:

1 Technical Paper Optimal Design of Integrated Missile Guidance and Control Lin, Ching-Fang, Ohlmeyer, Ernest, Bibel, John E., Malyevac, Steve Society of Automotive Engineers	7 Technical Paper Numerical SDRE Approach for Missile Integrated Guidance - Control S. Vaddi, P. Menon, E. Ohlmeyer American Institute of Aeronautics and Astronautics
2 Technical Paper GPS-aided navigation system requirements for smart munitions and guided missiles Ohlmeyer, Ernest J., Pepitone, Thomas R., Miller, B. Larry, Malyevac, D. Stephen, Bibel, John E., Evans, Alan G. American Institute of Aeronautics and Astronautics	8 Technical Paper Guidance, Navigation and Control Without Gyros: A Gun-Launched Munition Concept Ohlmeyer, E., Fraysse, J., Pepitone, T. American Institute of Aeronautics and Astronautics
3 Technical Paper Guidance Law Design for Missiles with Reduced Seeker Field-of-View M. Xin, S. Balakrishnan, E. Ohlmeyer American Institute of Aeronautics and Astronautics	9 Technical Paper Guidance, Navigation and Control System Design for a Tri-Propeller VTOL UAV J. Althaus, Y. Liu, R. Huang, N. Daniher, C. Engel, J. Zhu American Institute of Aeronautics and Astronautics
4 Technical Paper Root-mean-square miss distance of proportional navigation missile against sinusoidal target Ohlmeyer, E. American Institute of Aeronautics and Astronautics	10 Technical Paper Comparison Between Three Spiraling Ballistic Missile State Estimators J. Kim, S. Vaddi, P. Menon, E. Ohlmeyer American Institute of Aeronautics and Astronautics
5 Technical Paper Nonlinear Discrete-time Design Methods for Missile Flight Control Systems Menon, P., Sweriduk, G., Vaddi, S., Ohlmeyer, E. American Institute of Aeronautics and Astronautics	11 Technical Paper Nonlinear Integrated Guidance-Control Laws for Homing Missiles Menon,P., Ohlmeyer,E. American Institute of Aeronautics and Astronautics
6 Technical Paper Target State Estimation for Integrated Guidance-Control of Missiles S. Vaddi, P. Menon, E. Ohlmeyer American Institute of Aeronautics and Astronautics	12 Technical Paper Nonlinear Bank-to-Turn/Skid-to-Turn Missile Outer-Loop/Inner-Loop Autopilot Design with theta-D Technique Xin, M., Balakrishnan, S., Stansbery, D., Ohlmeyer, E. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12