Repid Near-Optimal Trajectory Generation and Guidance Law Development for Single-Stage-to-Orbit Airbreathing Vehicles

Repid Near-Optimal Trajectory Generation and Guidance Law Development for Single-Stage-to-Orbit Airbreathing Vehicles

Author(s):

Calise, A.J. ( Georgia Insititute of Technology )
Flandro, G.A.
Corban, J.E.
Moerder, D.D.

Publication title:

NASA Technical Reports

Pub. Year:

1990

Issue:

NASA-CR-186299

No.:

G3/18 0260650

Pt.:

NAS 1.26:186299

Paper no.:

N90-19275

Page(from):

1

Page(to):

69

Pages:

69

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:	ZA00001426
Note for article:	NAG-1-922

Similar Items:

1 Technical Paper Rapid Near-Optimal Aerospace Plane Trajectory Generation and Guidance Calise, A.J. National Aeronautics and Space Adminstration	7 Technical Paper Guidance law development for aeroassisted transfer vehicles using matched asymptotic expansions Calise, Anthony J., Melamed, Nahum National Aeronautics and Space Adminstration
2 Technical Paper Reusable Launch Vehicle Adaptive Guidance and Control Using Neural Networks Johnson,E., Calise,A., Corban,J. American Institute of Aeronautics and Astronautics	8 Technical Paper Optimal Guidance Law Development for an Advaced Launch System : INTERIM PROGESS REPRT Calise, Anthony.J., Hodges, Dewey.H. National Aeronautics and Space Adminstration
3 Technical Paper Nonlinear Feedback Guidance Law for Areo-Assisted Orbit Transfer Maneuvers Menon, P.K.A., Dr., Moerder, D.D., Dr. National Aeronautics and Space Adminstration	9 Technical Paper A Six Degree-of-Freedom Adaptive Flight Control Architecture for Trajectory Following Johnson, E., Corban, J., Calise, A. American Institute of Aeronautics and Astronautics
4 Technical Paper Hybrid near-optimal aeroassisted orbit transfer plane change trajectories Calise, Anthony J., Duckeman, Gregory A. National Aeronautics and Space Adminstration	10 Technical Paper Operability Sensitivities of Airbreathing and Rocket Propulsion for a Two-Stage-to-Orbit Space Operations Vehicle (SOV). Hatakeyama, S.J., Mclver, K.L., Embler, J.D., Gillard, W.G. American Institute of Aeronautics and Astronautics
5 Technical Paper Life Cycle Analysis of a Single Stage to Orbit (SSTO) Reusable Launch Vehicle Robinson, J.S., Culver, G.A., Bishop, R.D., Bright, E.D. American Institute of Aeronautics and Astronautics	11 Technical Paper Analytical investigations in aircraft and spacecraft trajectory optimization and optimal guidance Markopoulos, Nikos, Calise, Anthony J. National Aeronautics and Space Adminstration
6 Technical Paper Optimal Guidance Law Development for an Advanced Launch System Calise, Anthony J., Leugh, Martin S.K. National Aeronautics and Space Adminstration	12 Technical Paper The Possibility of Near-Term Commercial Single-Stage-To-Orbit Vehicles Dorrington, G. E. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12