Recent advances in the solution of large nonlinear optimization problems with WORHP

Engineering Optimization IV - Proceedings of the 4th International Conference on Engineering Optimization, ENGOPT 2014

Emergency Flight Replanning to Minimize the Risk of Loss of Life Using a Decoupled Trajectory Optimization Approach

2013 Aviation Technology, Integration, and Operations Conference

In-Flight Emergency Flight Planning Using a Decoupled Trajectory Optimization Technique

CEAS2013: "Innovative Europe", 16.09. -19.09.2013, Linköping, Sweden

Lattice Boltzmann Constraints for Standard Optimization Problems

PAMM

LQR Control for a Diesel Engine's Air System

PAMM

Modeling and Optimization in Space Engineering

Nonlinear Parameter Identification for Ordinary Differential Equations

PAMM

The ESA NLP solver WORHP

Springer Optimization and Its Applications

Benefits of Optimal Flight Planning for Noise and Emissions Reduction at Frankfurt Airport

AIAA Guidance, Navigation, and Control Conference, August 13–16, 2012, Minneapolis, USA

Benefits of Optimal Flight Planning for Noise and Emissions Reduction at Frankfurt Airport

AIAA Guidance, Navigation, and Control Conference 2012

Real-Time Trajectory Synthesis Using Multivariate Interpolation Methods: The Case of a Lunar Landing Maneuver

61st German Aerospace Congress, September 10–12, 2012, Berlin, Germany

From WORHP to TransWORHP

5th International Conference on Astrodynamics Tools and Techniques, May 29–June 1, 2012, Noordwijk, Netherlands

SVAGO MDO environment for the design of expendable launch vehicles

5th International Conference on Astrodynamics Tools and Techniques, May 29–June 1, 2012, Noordwijk, Netherlands

WORHP - The ESA NLP Solver

5th International Conference on Astrodynamics Tools and Techniques, May 29–June 1, 2012, Noordwijk, Netherlands

Emission-Optimal Flight Trajectories with Weather Hazard Avoidance and 4D Wind Modeling

3rd CEAS Air & Space Conference, October 24–28, 2011, Venice, Italy

Global and Local Multidisciplinary Design Optimization of Expendable Launch Vehicles

7th AIAA Multidisciplinary Design Optimization Specialist Conference, April 2011, Denver, USA

Global and Local Multidisciplinary Design Optimization of Expendable Launch Vehicles

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Conference on Structures, Structural Dynamics, and Materials

Global and Local Optimization Approaches for the Design of Launch Vehicle Ascent Trajectories

62nd International Astronautical Congress 2011, IAC 2011

Multidisciplinary Optimization of Launch Vehicles: A Step From Conceptual to Early Preliminary Design

62nd International Astronautical Conference, October 3–7, 2011, Cape Town, South Africa

Nonlinear Optimization in Space Applications Using WORHP

62nd International Astronautical Congress 2011, IAC 2011

On-Board Trajectory Optimization of RNAV Departure and Arrival Procedures with Regard to Emissions and Noise Disturbance to Residents

Optimal Guidance and Control of Lunar Landers with a Non-Throttable Main Engine

1st CEAS Specialist Conference on Guidance, Navigation, and Control, April 13–15, 2011, Munich, Germany

Post-Optimal Sensitivities of Flight Trajectories with Respect to Selected Parameters

1st CEAS Specialist Conference on Guidance, Navigation, and Control, April 13–15, 2011, Munich, Germany

Real-time control of optimal low-thrust transfer to the Sun-Earth L(1) halo orbit in the bicircular four-body problem

Acta Astronautica

Suboptimal Control of Nonlinear Processes

at - Automation technology